self-similar solutions as intermediate asymptotics …hunter/m207c/barenblatt.pdf · 286 barenblatt...

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Copyright 1972. All rights reserved SELF-SIMILAR SOLUTIONS AS INTERMEDIATE ASYMPTOTICS G. I. BARENBLATT Institute of Mechanics, Moscow University, Moscow, USSR YA. B. ZEL’DOVICH institute of Applied Mathematics, USSR Academy of Sciences, Moscow,USSR INTRODUCTION Hydrodynamics, like other branches of continuum mechanics, has long been dealing with particular solutions of the special type m(t)F[x/l(t)], where x and t are independent variables that may]someUmes.}be interpreted as a spatial coordinate and time, and re(t) and l(¢) are time-dependent scales of the unknown variable and the spatial coordinate. The name of these solu- tions, self-similar, comes from the fact that the spatial distribution of the characteristics of motion, i.e., of the dependent variables, remains similar to itself at all times during the motion. Self-similar solutions always represent solutions of degenerate problems for which all constant parameters entering the in]’,tlal and boundary conditions and having the dimensions of the inde- pendent variables vanish or become infinite. Interest in self-similar solutions was originally due to the fact that they are representable in terms of functions of one variable. Hence the solution of partial[ differential equations for the corresponding problems is reduced to the solution of ordinary differential equations, and this was thought to be simpler according to the hierarchy of complexity existing at that time. By this means it was possible,to obtain a numberof exact special solutions, sometimes even in analytic form. F.or linear equations, the principle of super- position is valid and these exact solutions can be used directly in construct- ing solutions of more general problems, such as the self-similar fundamental solution of the inltial-value problem for the heat-conductlon equation. But what is the place of self-slmilar solutions in the case of the general nonlinear problem? Muchlater it was realized that self-slmilar solutions do not represent merely specific examples. In actual fact they describe the "intermediate- asymptotic" behavior of solutions of wider classes of initial, boundary, and mixed problems, i.e., they describe the behavior of these solutions away from the boundaries of the region of independent variables or, alternatively, in the region where in a sense the solution is no longer dependent on the de- tails of the initial and/or boundaryconditions but the system is still far from being in a state of equilibrium. 285 8026 www.annualreviews.org/aronline Annual Reviews

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Page 1: SELF-SIMILAR SOLUTIONS AS INTERMEDIATE ASYMPTOTICS …hunter/m207c/barenblatt.pdf · 286 BARENBLATT & ZEL’DOVICH The development of computers has also changed the attitude toward

Copyright 1972. All rights reserved

SELF-SIMILAR SOLUTIONS AS INTERMEDIATEASYMPTOTICSG. I. BARENBLATT

Institute of Mechanics, Moscow University, Moscow, USSR

YA. B. ZEL’DOVICH

institute of Applied Mathematics, USSR Academy of Sciences, Moscow, USSR

INTRODUCTION

Hydrodynamics, like other branches of continuum mechanics, has longbeen dealing with particular solutions of the special type m(t)F[x/l(t)],where x and t are independent variables that may]someUmes.}be interpretedas a spatial coordinate and time, and re(t) and l(¢) are time-dependent scalesof the unknown variable and the spatial coordinate. The name of these solu-tions, self-similar, comes from the fact that the spatial distribution of thecharacteristics of motion, i.e., of the dependent variables, remains similar toitself at all times during the motion. Self-similar solutions always representsolutions of degenerate problems for which all constant parameters enteringthe in]’,tlal and boundary conditions and having the dimensions of the inde-pendent variables vanish or become infinite.

Interest in self-similar solutions was originally due to the fact that theyare representable in terms of functions of one variable. Hence the solution ofpartial[ differential equations for the corresponding problems is reduced tothe solution of ordinary differential equations, and this was thought to besimpler according to the hierarchy of complexity existing at that time. Bythis means it was possible,to obtain a numberof exact special solutions,sometimes even in analytic form. F.or linear equations, the principle of super-position is valid and these exact solutions can be used directly in construct-ing solutions of more general problems, such as the self-similar fundamentalsolution of the inltial-value problem for the heat-conductlon equation. Butwhat is the place of self-slmilar solutions in the case of the general nonlinearproblem?

Much later it was realized that self-slmilar solutions do not representmerely specific examples. In actual fact they describe the "intermediate-asymptotic" behavior of solutions of wider classes of initial, boundary, andmixed problems, i.e., they describe the behavior of these solutions awayfrom the boundaries of the region of independent variables or, alternatively,in the region where in a sense the solution is no longer dependent on the de-tails of the initial and/or boundary conditions but the system is still far frombeing in a state of equilibrium.

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286 BARENBLATT & ZEL’DOVICH

The development of computers has also changed the attitude towardself-slmilar solutions. Indeed, in simple cases the reduction of a partial dif-ferential equation to an ordinary equation makes it possible to obtain thesolution in an elementary way. In more complex problems, however, whenthe construction of a self-similar solution leads to a boundary-value problemfor a system of ordinary equations with conditions at different ends of an in-finite interval, the most efficient method of obtaining the solution is not tosolve the boundary-value problem for the system of ordinary equations di-rectly but to return to the partial differential equations and to follow in aspecific instance the passage of the solution into a self-similar intermediateasymptotlcs. Thus, in practice self-similarity is of interest not because it, as itwere, facilitates the calculation, but because it reflects an important propertyof the process at hand, which is obscured by accidental details of the initialand boundary conditions)

The treatment of self-similar solutions as intermediate asymptotics en-ables one to clarify fully the role of dimensional analysis in their construc-tion. Indeed, in many cases the self-similarity of intermediate asymptoticscan be established and the form of self-similar intermediate asymptotics ob-tained from dimensional considerations. This is far from always so, however.Self-similarities obtained from dimensional considerations, i.e., self-similarsolutions of the first type, form only the visible top of the iceberg. The pointis that actually the use of dimensional analysis tacitly assumes a certainregularity of the limiting process in passing from the original non-self-similarsolution of a nondegenerate problem to a self-similar intermediate asymptot-ics, i.e., to the solution of the degenerate problem. In many cases, however,the passage to the limit is not regular. In such cases dimensional analysis isfound to be inadequate to establish the form of a self-similar intermediateasymptotics, and dimensional considerations must be supplemented by thesolution of a certain eigenvalue problem that is, generally speaking, non-linear. Thus arise the so-called self-similar solutions of the second type.

Moreover, in some cases dimensional analysis is inadequate to establishthe self-similarity of an intermediate asymptotics, since this self-similarity issometimes related to the invarlance of the statement of the correspondingdegenerate problem with respect to a wider group of transformations thanthe group of similarity transformations of quantities with independentdimensions.

Of special interest is the recently discovered intimate relationship be-tween self-similar solutions and uniform-propagation regimes. The uniform-

1 This idea is best expressed by the Russian poet Alexander Blok in his poem

"The Retribution":Co~p~ cay~at~H~e ~epw~--

1~ w~I y~l~mr,: ~at~p nper~pace~.

(Obliterate the accidental features--And you will see: the world is splendid.)

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SELF-SIMILAR SOLUTIONS 287

propagation regime is a solution of the formf(x-X~2cc) such that the solu-tion at the next instant is obtained by a shift in coordinate from the solutioncorresponding to the preceding instant. In the exact, degenerate, statementof a problem, such solutions occur for equations that do not explicitly con-tain x and t, with boundary conditions at + ¢o and - oo. For these problems,questions also arise as to the passage of the solution under arbitrary initialconditions into an intermediate-asymptotlc unlform-propagatlon regime, aswell as to a classification of regimes, analogous to the classification of self-similar solutions into solutions of the first and second type.

Self-similar solutions of the first type, whose existence is related only tothe conservation laws and to the invariance of the degenerate problem withrespect to the group of si~nilarity transformations of quantities with inde-pendent dimensions are well known. We may mention here a self-similarstrong explosion (Sedov 1946, 1967, Taylor 1950) and a thermal wave(Zel’dovich & Kompaneets 1950, Barenblatt 1952, Zel’dovich & Raizer1963). In the present review, primary emphasis is placed on self-similar solu-tions of the second type; we turn to self-slmilar solutions of the first typeonly episodically when continuity and contrasts are concerned.

SELF-SIMILAR SOLUTIONS OF FroST ANY SECOND TYPE

Example: Modified problem of a strong explosion.--An example of a self-similar intermediate asymptotlcs is provided by the phenomena occurring atthe initial stage of a nuclear explosion.

At the very first stage, immediately following energy release, thermalwaves are propagated in as yet stationary gas; heat conduction is then de-termiued mainly by radiation.2

The rate of transfer of energy by radiation decreases with time and ulti-mately becomes small in comparison with the speed of sound; then therecomes the next stage where it is necessary to consider the motion of the gas,which may be assumed to be adiabatic. In the heated gas, the pressure in-creases greatly with the result that a strong shock wave is generated andpropagated through the gas (the pressure at the shock front being severalorders higher than the initial gas pressure). When the shock wave overtakesthe thermal wave (their common radius is taken to be R0 at that instant), thehydrodynamic stage of the explosion sets in. At this stage, the solution alsodepends on the total amount of released energy E, the initial gas pressureP0, and its initial density p0; it has the following parameters with dimen-sions of length: Ll=(E/po) 11~, L2=R0, and with dimensions of time:(poE21~l/po~la)~12, t~= (poRo~/E)~12. For the conditions of a nuclear explosion,Lt>>L~ and t~>>t2. The intermediate asymptotic regime corresponding to thestage of strong shock waves was discovered and studied by Sedov (1946) and

~ Transfer of energy by radiation at the initial stage occurs at a rate many timesthe speed of sound so that the hydrodynamic displacement of substance at this stagecan be neglected.

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Taylor (1950); the self-similar intermediate asymptotics obtained by them valid for LI>>r>>L~ and tl>>t))t2. The corresponding expressions for thecharacteristics of the motion (velocity v, density p, and pressure p) are

v =-- v(~), ~ = po~(O, ~ = ~o ~ ~(0, ~t (Et~/oo)~

where P, V, and R are functions of one variable ~ (the exponent of the adi-abatic curve ~ being a parameter of the p~oblem) satisfying a system ofordinary differential equations and boundary conditions that are obtainedby substitution of expressions (1) into the gas-dynamic equations and theboundary conditions, simplified on the assumption that shock waves arestrong (i.e., that the initial pressure can be neglected in comparison with th~pressure behind the shock front); these functions are found in finite form.

The self-similar intermediate-asymptotic regime considered above in-volves the energy integral, which is also valid for non-self-similar stages ofthe motion when the details of the initial and boundary conditions are stillimportant. Hence the self-~imilarity of the solution and its representationin the form of (1) can be obtained from dimensional analysis, i.e., from theinvarlance of the intermediate asymptoties with respect to a subgroup of th~group of similarity transformations~the group of transformations of quan-tities with independent dimensions. The reasoning is as follows. As does anyintermediate asymptotics, relations (1) represent the solution (in the com-monly used terminology the exact solution) of a certain degenerate problem.In the case at hand, it is the solution of the Cauehy problem for the equationsof gas dynamics corresponding to singular initial data, viz to an instantane-ous release of a finite amount of energy E at a particular point. The desiredsolution of the degenerate problem, if it exists and is unique, can be de-termined by the independent variables, the parameters entering the equa-tions (insluding the conditions at the shock front), and the initial conditions,and only by them; for the problem of propagation of strong shock wavesduring a nuclear explosion, the solution is determined by the quantities E,00, t, r, ~. The solution cannot depend on the natural arbitrariness in thechoice of the basic units of measure and must be represented as a relationamong dimensionless quantities; therefore, in the problem of propagation ofstrong shock waves, the dimensionless quantities p/(oorVt~), 0/~o, andv/(r/t) can depend only on the dimensionless combinations of the governingparameters ~ =r/(E~/Oo)~ and ~ (no other dimensionless combinations ofthe quantities E, ~0, t, r, and ~ can be set up), whence representation (1) obtained.

The foregoing line of reasoning is typical and it is commonly thought thatthe derivation of self-similar solutions is always associated with dimensionalanalysis, so that by applying dimensional analysis and proeeedlng from thestatement of the degenerate problem whose exact solution is an intermediateasymptofics it is always possible to obtain a self-similar form of the inter-

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SELF-SIMILAR SOLUTIONS 289

mediate-asymptotic solution, expressions for the self-similar variable, and,as a result of the solution of the corresponding boundary-value problem forthe system of ordinary equations, the full solution, including the constantsinvolved.

This is indeed the case for a definite class of problems. The well-knownbook of Sedov (1967) contains a large collection of examples of this kind anda description of the general approach to be used in such cases. However,there exists a wide class of self-similar problems in which the self-similarity isestablished and exponents in the expressions for the self-similar variables aredetermined not from dimensional analysis of the degenerate problem butfrom consideration of the limiting passage from the original non-self-similarsolution to an intermediate asymptotics and, in particular, from the condi-tion for existence of the limiting self-similar solution in the large. Charac-teristic of these solutions is that they contain (one or several) dimensionalconstants that are not determined from the conservation laws but can befound by matching the self-similar intermediate asymptotics with non-self-similar solutions whose asymptotics they represent.

Such solutions have long attracted attention and received in the literaturethe special name self-slmilar solutions of the second type. These solutions arenot, under any circumstances, to be regarded as rare exceptions. Quite thereverse~they are frequently encountered but not always properly identi-fied.

The appearance of self-similar solutions of the second type as an inter-mediate asymptotics is due to a peculiar nonregularity of the limiting passagefrom the original non-self-similar solution to a self-similar intermediate-asymptotic regime. This can be seen by modifying somewhat the aboveproblem of the propagation of strong shock waves (see Barenblatt Zel’dovlch 1971, Barenblatt & Sivashinsky 1970). The modification consistsin assuming the exponent 3’ of the adiabatic curve in the continuous part ofthe flow behind the shock wave to be different from the parameter ~/1 thatenters the conditions at the shock front through the expression for theenergy: E=p(3,1--1)p. This situation with 3"1<3" occurs, for example, ifenergy is lost by radiation at the shock front with an intensity proportionalto the 3/2 power of the temperature, and the undisturbed gas is completelytransparent for radiation. If ~’--3"i, we have the previously discussed problemof propagation of strong shock waves, which leads to a self-slmilar solutionof the first type.

The parameters ~/and "y~ are dimensionless constants. This would seem toindicate, therefore, that the addition of the new governing parameter ~’1should not change anything, and the foregoing dimensional considerations,which apply to the degenerate problem and lead to solution (1), must hold.The fact that the inequality qq#3’ corresponds to radiation or (whenTx>3’) to energy release at the front means, however, that the energy con-tained in the disturbed region is no longer a constantl it cannot be equatedto the given initial energy of explosion. From this it is seen that the situation

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is radically changed. This can readily be verified formally. Indeed, if we sub-sfitute expressions (1) into the gas-dynamic equations and boundary condi-tions for the problem with

o,v + vorv = - orp/p, o,p + o,(pv) 2pv/r = 0 (2)O,(p/pO + "~dP/pO = 0 (3)2 2

~[,0(0 - o, t] = -- ~0D~, ,[,0(0 - 0, t] D,’,/~. + 1 ~/~ + I (4)

o[,o(t) o,t] = (~iwhere r0(0 and D are, respectively, the radius and velocity of the shockfront, we immediately come to a contradiction, so that there exists no self-similar solution in the form of (1) that would satisfy the required conditionswith 3q ~3’. In fact, the solution in the form (1) gives the following expressionfor the total energy

~ = p q- r~dr

So= E ~°R(~) + - ~d~ = const

where ~o=ro(t)/(Et~/po) ~1~, that is, de/dt=O. However the energy conditionat the shock wave being written in the form

p(v -- D) -t- q- pv = -3’--10 1

shows that

3"~-- ~ p(v-- D)

at r ---- ro(t) --

d, (~ - ~) p[,o(0 - o, t]-- = -- 4fronD p0 # 0dt (y -- 1)(3"x -- 1) p[ro(t) -- O, t]

The nonexistence of a self-similar solution in the form Of (1) means thatthe intermediate asymptotics of the solution of the original non-self-similarproblem has another form when 3’1 ~’Y.

To determine the intermediate asymptotics we consider the original non-self-similar problem: In a space filled with a gas at rest of density po there is aspherically symmetric domain of radius R0 in which at the initial time a finiteamount of energy/~ is instantaneously released according to a certain spher-ically symmetric law (by raising the gas temperature and producing a vel-ocity field). It may be assumed (though this is not proved) that the solution

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SELF-SIMILAR SOLUTIONS 291

of this non-self-similar problem exists and is unique. As before, the shockwave propagating through the gas and separating the disturbed region fromthe undisturbed one is considered to be strong, i.e., the initial gas pressure isneglected. In the non-self-similar problem, there are then two independentdimensionless variables

r R0~- (~t2/P°)l~°,

~ = (~t2/Po)’~ (5)

so that, by virtue of dimensional considerations, the solution of the equationsof gas dynamics is written as

0=00R(~,r, 3’,’~l), P=o0~P(~,r,y, yx), v =l--V(~’r’~’ra)

As a general guide, we consider the problem of propagation of a ztrongspherical shock wave by approximate means, using the equations for thefront radius ro(t), the pressure P and temperature T at the shock front, andthe mass of gas g and total energy E contained in the region encompassed bythe wave. All these quantities depend only on the time t with the followingrelations existing among them:

4 E E~ =~poro~ T = a~, P = boot = cpo~

dro

~

dE.....dt f ’ dt

where a, b, c, f, and g are constants.We focus our attention on the last equation, which describes the energy

radiation by the wave. The case ~=~ corresponds to g=0, E=constant,and leads to self-similarity of the first type. The coefficients a, b and c de-pend on the detailed structure of the solution (the dependence of the localpressure and temperature on the dimensionless ratio r/ro, the velocity dis-tribution for r <r0, etc.) ; their numerical values can be found only by solvingpartial differential equations. They also depend, of course, on the parameters~ and % However, the fact that the quantities a... g are time-independentwill be su~cient in what follows. We obtain in an elementary way

dro dE-- = hEXl~ro-31~’

-- = _ kEbl~ro-~12dt dt

dE E-- = -- n--, E = qro-~dro ro

where h, k, n, and ~/are constants. Thus the chosen law of radiation at the

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shock front leads to a power-law relation between energy and radius; thedimensionless exponent n depends on the dimensionless quantities ~’ and ~’1with n"~3"-q¢l for ~/-3"1<<1. From this we can now easily find power-lawrelations for other quantldes. For example,

dro

dt

We now turn to the consideration of the exadt solution. The well-knownsolution of the problem of a strong explosion (1) represents, on the one hand,an intermediate asymptotics that is obtained from the non-self-similar solu-tion (6) if 3’ =3’1, z-~0, and ~ is finite (i.e., if t--~ ~ for sufficiently large r), at the same time it represents the solution of the Cauchy problem withsingular initial data corresponding to R0 =0 (instantaneous release of a finiteamount of energy at a point). The nonexistence of the solution to the de-generate problem of instantaneous release of a finite amount of energy at apoint, i.e., the nonexistence of an intermediate asymptotics of the form of(1) when 3"1 #3", means that in this case no finite limit of the functions P andV exists for finite ~ and r--*0. Note that if t increases and r is finite, bothvariables, ~ and r, tend to zero. When 3’1 #3’ and ~, r--~0, the principal termsof the asymptotic representations of the function _P, V~ and /~ are supposedto be

where X is a real number different from zero when 3"z #3". Hence the resultantlimiting solution corresponding to the intermediate asymptotic regime is alsoself-similar and is given by

p = p(~-),

At~ ’

v = v(r), n = R (/9,

P0

(8)

where a = 2(1 -),)/5 = 2/(n+5) ; the constant factor ~ is introduced to ~ equal to unity at the shock front.

Thus when 3’~ #’r the intermediate asymptofics is no longer a solution ofthe degenerate problem of gas motion under the action of an instantaneouslyreleased finite amount of energy at a point. The solution appropriate to theintermediate asymptotics corresponds to the instantaneous release of anamount of energy E in an infinitesimal domain of radius R0, which tends tozero or infinity as R0-~0 according to the value of X, so that

ER05x/(1-x) = const (9)

When 3"1 <% which corresponds to energy radiation at the shock front, X >0and E--~ oo as Ro--~O.

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SELF-SIMILAR SOLUTIONS 293

It may be said that when ~v~’ the intermediate asymptotics "re-members" neither the energy E nor the size R0 of the domain in which theenergy is released at the initial time but a combination of these quantitieswith transcendental dimensions in general. The exponent ~, or, what amountsto the same thing, the exponent a of the time in the expression for the self-similar variable, which gives the dimensions of the constant A, is determinedexclusively by the quantities ~ and ~ and is independent of the initialconditions. On the other hand, the numerical value of the constant A re-mains as an "imprint" of the limiting passage from the original non-self-similar solution to the self-similar intermediate asymptotics. The quantityA, a constant entering the self-similar intermediate asymptotics, remains, ofcourse, the same for the entire non-self-similar motion (the state at any timemay be taken as the initial one) and in this sense is its "integral" (cf Lax1968). When 3"1 #3’ it is impossible, however, to indicate an integral of theinitial distribution of quantities of the original non-self-similar problem thatwould give a value for A in the same manner as the energy integral in the caseof’rt--3’: the "integral" A is in this case a more complicated functional. When3’1 =% k = 0, and a--2/5, the limiting passage to an intermediate asymptoticsis regular and a self-similar solution of the first type is obtained.

The determination of the parameter k represents a peculiar eigenvalueproblem. Substituting the representation of the solution (8) into the system(2)-(4) and bearing in mind that to(t)=At e and D=Aat~-I, we obtain anonlinear eigenvalue problem for the determination of X. The parameter X isthus found from the condition for existence of a self-similar solution of theform of (8) in the large. It can be shown that when 3"<2 and 3"i<23"+1the eigenvalue of the problem X=X0 is uniquely determined; on the otherhand, when qet>2~,+l the eigenvalue is not uniquely determined. Theconstant A cannot in principle be determined from eonsideratlon of theself-similar solution alone; to find it, it is necessary to follow (numerically,for example) the evolution of a non-self-similar solution up to its transitioninto the intermedlate-asymptotlc regime. The presence of an undeterminedconstant implies a certain nonautonomy of the intermediate asymptotlcs,i.e., the overall effect of the non-self-similar problem on the self-similar inter-mediate asymptotlcs, which is not determined by the integral conservationlaws.3

~ The nonautonomy of the intermediate-asymptotic regime may also be en-countered in cases where these regimes represent self-similar solutions of the firsttype. An illustrative example is provided by the Cauchy problem for the nonlinearheat-conduction equation (Barenblatt 1956):

O~T = ~r-~,(r~T~&T), T(r, O) = ~r~(r < Ro), T(r, O) -- ~Ro~(r

It is natural to expect that for small values of r and t an asymptotic regime exists.If r<<Ro, it may be assumed that the asymplotic regime is described by a self-similarsolution of the Cauchy problem corresponding to the initial condition T(r, O)= e

(a>0, 0_<r < ~o). Dimensional analysis shows that this solution represents a self-

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Uniform propagation regimes and their relation to self-similar solutions.-The above example of the self-similar intermediate asymptotics in the modi-fied problem of a strong explosion is representative in the sense that inthis example the asymptofics is in general (i.e., when TI~T) described by self-similar solution of the second type, while for one value of the parameter(’Ix ~’I) a self-similar solution of the first type is obtained. At present manyproblems are known that lead to self-similar solutions of the second type;some of these will be discussed below. Here we shall consider the funda-mental work of Kolmogorov, Petrovsky & Piskunov, accomplished back in1937. In this remarkable work, the ideas of invariant intermediate asympto-tics were first expressed in clear form with reference to uniform propagationregimes, and the treatment was carried through to the final stage for theproblem dealt with in that work. As we shall see later, this work containedessentially the concept of self-similar solutions of the second type.

Kolmogorov, Petrovsky & Piskunov (1937) considered, as applied to thebiological problem of spatial propagation of gene which has the advantage innatural selection, the nonlinear equation with the right-hand side

o,v - kO~v -- F(v) (10)

where F(v) is a continuous and differentiable (as many times as may be quired) function defined in the interval 0_<v ((1 and has the following pro-perties:

F(0) = F(1) F(~) > 0 (0 < ~ < (11)

F’(0) = ~ > F’(v) < ~ (~ > These authors showed that Equation (10) has solutions of the type of uni-formly propagating waves ("stationary solutions")

v = v(~ + xt +c) (12)where c is an arbitrary real number, which satisfy the conditions V(- ~o) and V(~)= 1 for all velocities of propagation )t greater than )to =2~/k~.

similarity of the first type and is expressed in terms of the solution of a boundary-value problem for an ordinary nonlinear equation. The solution of this boundary-value problem is unique only if 0_~ a < 2 In; if a :> 2 In, it is not unique. The solutionin the second case is determined to within a constant, which can be found by followingthe transition of the solution of the non-self-similar problem into the self-similarasymptotic regime. This means just the presence, if ~ 2/n, of the overall effect (interms of one constant, which is not determined from the integral conservation laws)of the initial temperature distribution at distant points on the self-similar asymptoticregime near the center of symmetry, i.e., the nonautonomy of this regime, which isdue to the inflow of heat from outside. If 0 <a <~2/n, the solution is unique and theself-similar asymptotic regime is autonomous. The self-slmilar asymptotic regimetakes place when 0 <t<<Ro~-~"(~a’~)-~ (the rlght-hand side of the inequality containingthe unique characteristic time of the problem) ; as is seen, if a >2/n the time of exis-tence of the intermediate asymptotic regime decreases with increasing Ro.

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SELF-SIMILAR SOLUTIONS 295

However, among the solutions (12) only the solution corresponding to theminimum velocity of propagation X --X0 can be an asymptotics at t--+ oo of thesolution of the Cauchy problem corresponding to the initial data

V(~, 0) ~- (~ < a)

o < v(x, o) < (a < x < b) (13)

V(x, o) =- (x > b)

where a and b (a<b) are arbitrary real numbers and Ozv(x, 0)>0. In otherwords, the direct consideration of stationary solutions in the large leads to acontinuous spectrum of possible velocities of propagation ~ _~)~0, but only thesolutions corresponding to the extreme point of the spectrum ~ =~0 can beasymptotics of the nonstationary solution of the Cauchy problem as t--~The constant c remains undetermined when only stationary solutions areconsidered; to find it, it is necessary to follow (numerically, for example) thedevelopment of the nonstationary solution of the Cauchy problem up to itstransition into the stationary regime.

It remained surprisingly unnoticed that the problem of constructing self-similar solutions of the second type was basically the same as the problem ofuniform propagation regimes with a velocity unknown in advance, whichwas considered by Kolmogorov, Petrovsky & Piskunov (1937). Indeed, if transform to the independent variables ~=ex and v=e-~, the solutions (12)can be represented in the self-similar form

v ---- V(ln $ -- X In r’b c) = U(~/Ar~) (14)

where A--e-¢. The foregoing results are formulated in self-similar terms asfollows:

1. The equation obtained from Equation (10) by a change of variables,

¯ oTv + ~o~v + ~o~v + F(v) = 0 (15)has self-slmilar solutions of the form v = U(~/AvX), which satisfy the condi-tions U(0)=0 and U(oo)--1. The condition for existence of the self-similarsolution in the large results in a continuous spectrum of values of the ex-ponent X >X0 in the expression for the self-similar variable ~/Avx.

2. The value ~ =~0 is selected by the additional requirement of stabilityin the sense that a self-similar solution must represent an asymptotics, asz--~0, of a certain class of solutions of the non-self-similar Cauchy problem.

3. The constant A remains undetermined when only self-similar solu-tions are considered; to find it, it is necessary to follow (numerically, forexample) the passage of the solution of the non-self-similar problem into theself-slmilar intermediate asymptotlcs. Thus, in the new variables the station-ary solutions considered by Kolmogorov, Petrovsky & Piskunov (1937)represent an example of self-slmilar solutions of the second type.

The idea of asymptotic uniform-propagation regimes with a velocity

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296 BARENBLATT & ZEL’DOVICH

unknown in advance, which was formulated by Kolmogorov, Petrovsky &Piskunov (1937), proved to be very fruitful in many problems. Here we men-tion first the theory of combustion, where this idea was applied to developthe theory of normal flame propagation (Zel’dovleh & Frank-Kamenetsky1938, Zel’dovich 1948). In the statement of the problem adopted in the firstworks, the eigenvalue was uniquely determined from the condition for exist-ence of the uniform-propagation regime in the large; more general statementsof the problem, which lead in some cases to a nontrivial structure of theeigenvalue spectrum, may be found in Hirsehfelder & Curtiss (1949), yonK~rm~n & Penner (1954) and Gel’land (1959). Further, the idea of uniformpropagation regimes was applied in the consideration of the propagation of alaser spark (Bunkin et al 1969, Raizer 1970), the ionization wave (Barmin Kulikovsky 1969), and many other problems. Of particular note are theseries of investigations carried out recently by Raizer, which systematicallyuse the idea of uniform-propagation regimes in problems of high-frequencygas discharge and other analogous problems involving simultaneous con-sideration of the heat-conduction equation and Maxwell’s system of equa-tions (Raizer 1968, 1969, 1971). All these intermediate-asymptotic uniform-propagation regimes, in which the velocity of propagation is not determinedfrom the conservation laws but is found from simultaneous consideration ofthe conservation laws and the internal structure of the transition regime inthe above sense, correspond to self-similar solutions of the second type. Self-similar solutions of the first type in the same sense correspond to inter-mediate-asymptotic uniform-propagation regimes in which the velocity ofpropagation is determined from the conservation laws alone, without re-course to the internal structure of the transition regime. An example isprovided by shock waves in gas, or a still simpler example is furnished by thestationary solution of the Burgers equation

(the Burgers shock wave). It is easy to see that this equation has a solutioncorresponding to the uniform-propagation regime

u= U(x- Xt + c)

Here the velocity of propagation X is uniquely determined from the conserva-tion law

2

where u+=u(oo, t) and u_=u(- ~o, t), and is independent of the internalstructure of the shock wave, i.e., of the viscosity v. By transforming to thevariables ~--e" and r =e¢, we obtain a self-similar solution of the first type.Note that the reduction of self-slmilar solutions to uniform-propagationregimes was used by Stanyukovich (1955).

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SELF-SIMILAR SOLUTIONS 297

FIGURE 1. The near-apex asymptotics of the ideal incompressible flow pasta wedge gives rise to a self-similarity of second type.

Examples of self-similar solutions of the second type.--We shall discusshere several self-similar solutions of the second type, which are instructivefor different reasons.

The simplest and at the same time most fully representative self-similarsolution of the second type is obviously the well-known solution of the prob-lem of plane-potential flow of an ideal incompressible fluid within a corner.Consider the plane flow of an ideal fluid past a wedge in the form of anisosceles triangle with an angle at the vertex of 2a; the velocity at infinity isparallel to the line of symmetry of the wedge and is equal to U (Figure 1).The velocity potential ~ satisfies Laplace’s equation with obvious boundaryconditions and, from dimensional considerations, can be represented asdO = Urf(O, L/r)i where 0 is the polar angle, r the distance from the wedgevertex, and f a dimensionless function of its dimensionless arguments. Nomatter how great L/r, that is, how small the neighborhood of the wedgevertex we are interested in, we cannot disregard the second argument of thefunctionf and consider the degenerate problem of flow past an infinite wedgewith velocity U at infinity for determining an asymptotics, since no finitelimit of f(O, 7) exists as ~ =L/r--~ ~o. In this simplest problem the completenon-self-similar solution is easily found in closed form. It can readily beshown that for large values of 7,

f(O, 7) = ~x¢(0) + small quantities

Thus the principal term of the asymptotics of the potential near thewedge vertex, by itself a solution of Laplace’s equation, is of the formr# =Arl-Xdp(O), where A = ULx. The elgenvalue X is found directly by sub-stltution of this expression for the potential in Laplace’s equation from the

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298 BARENBLATT & ZEL’DOVICH

FIGURE 2. The asymptotics at infinity of the slow viscous incompressible flowcreated by a distributed source in a corner gives rise to a self-similarity of the first typeif a <a,~.0.715~r and to a self-similarity of the second type if a >a,.

condition for existence of a solution in the large, i.e., a solution for which thecircumferential component of the velocity vanishes when 0= +_a or 0= ___~rand only on these straight lines. The point of the spectrum for which thesolution satisfies all these conditions is uniquely found as h = --a/(~r--a).The constant A remains undetermined when only the self-similar solution isconsidered and must be found by matching with the original non-self-similarsolution.

To Sternberg & Koiter (1958) belongs a remarkable result that clearlyillustrates the appearance of self-similar solutions of the second type. Wepresent this result with reference to slow flow of a viscous fluid (Sternbergand Koiter studied a mathematically equivalent problem in the theory ofelasticity). ~ We consider the steady-state plane Stokes flow of a viscous in-compressible fluid corresponding to a source of strength Q placed at the ver-tex of a corner formed by two semi-infinite straight lines that form an angleof 2a (Figure 2). The solution to this problem was obtained by Jeffery (1915) the equivalent solution in the theory of elasticity was indicated somewhatearlier by Carothers (1912). It is self-similar and is determined by the follow-ing expression for the stream function ~k (the solution of the biharmonicequation AA~ =0):

4 The general consideration of self-similar solutions of the plane problem of elas-ticity and the plane problem of slow flo~v of a viscous fluid was accomplished byWilliams (1952) and Moffatt (1964). It is interesting to note that the analysis mathematically equivalent problems of plane elasticity and slow flow of a viscousfluid has been carried out for about sixty years practically without proper correlationso that the same difficulties are invariably overcome twice.

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SELF-SIMILAR SOLUTIONS 299

Q (20 cos 2a - sin 20)~ = - -- (16)

2 (sin 2a - 2a cos 2a)

which may be obtained by application to the problem under consideration ofthe usual procedure of dimensional analysis.

Sternberg and Koiter pointed out the paradoxical property of this solutionthat for a =a*~--- 0.715~r the denominator of expression (16) becomes zero, that the stream function becomes infinite at all points of the field.

To resolve the paradox, Sternberg and Koiter considered the followingnon-self-similar problem: In stralght-line portions of the boundary of acorner 0-- +a is given a symmetric distribution of normal velocities differentfrom zero for 0_<r_<a:

v0 = _+-- Q ~(p), p = --, ~(p) --- 0 (p _ > (17)2a a

For r:> 1 the condition of attachment is fulfilled, that is, both components ofthe velocity vanish, the tangential component of the velocity v~ is zero on theentire boundary of the corner; the total amount of fluid flowing into thecorner per unit time is Q, that is, fol~(p)dp = 1. The non-self-similar problemstated by Sternberg and Koiter was found to admit a solution in closed formby means of Mellin transformation. From dimensional considerations itfollows that the solution is representable as

~ = 0/(0, 7) (is)

where ~l=a/r and f is a dimensionless function of its dimensionless argu-ments.

It is natural that the solution of the degenerate problem corresponding tothe source placed at the vertex of the corner has meaning only if it is obtainedas the limit when the "portion of injection" O<_r<_a is contracted to zerowith the total rate of flow Q maintained constant or, which amounts to thesame thing, when r tends to infinity, i.e., when ~/--~0, i.e., if it is an inter-mediate asymptotics of the nonself-similar problem.

Based on their solution of the non-self-similar problem Sternberg andKoiter established the following:

1. If the vertex angle a is less than the limiting value, ot,~a>0, thelimit of the functionf(O, ~1) as ~/--~0 exists, is finite, and is equal to

1 (20 cos 2a -- sin 20)

2 (sin 2a -- 2a cos 2a)

so that the intermediate asymptotics is actually described by the Carothers-Jeffery solution and is a self-similar solution of the first type.

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300 BARENBLATT & ZEL’DOVICH

2. If the vertex angle ~ is greater than the limiting value, ~, Ks ~r, nofinite limit of the funetlonf(0, ~/) exists as ~/-~0, but instead

1 (20 cos 2a -- sin 20)7) -- + -- + o(1) (19)

2 (sin 2a -- 2c~ cos 2a)

where

(20)[(X + 2) cos (X + 2)a sin ~0 -- ~ cos Xa sin (X +

4X[sin 2a -- 2a cos 2(X -t- 1)a]

and X is the root of the equation

(~ q- 1) sin 2a -- sin 2(X q- 1)a (21)

that lies in the interval --1 <~ <0. Thus the principal term of the inter-mediate asymptotics of the stream function is represented in this case by theself-similar solution of the second type

o)= e (o, (22)

rather than by the Carothers-Jeffery solution. Here again, the exponent X isfound not from d~mens]onal considerations but from the conditions for ex[s-tence of the self-similar solution in the large. Substituting ~ given by theexpression ~=A~X¢(O, a) into the biharmonic equation, which must besatisfied by the stream function of slow flow, and using the conditions ¢=0~ =0 at 0 = ~a, which follow from the condition for attachment, we ob-tain a spectrum of eigenvalues X. If a. <a <~, the lowest e[genvalue is nega-tive and is less than unity in modulus. The constant A cannot be found fromth~s cons{dera~on. Formula (20) {nd[cates that [t is propor~onal to folpx

~(p)dp, that is, it depends on the prelimifing non-self-similar problem. Thusif a, <a <v the intermediate asymptotics "remembers" not the total flowrate Q and not the dimension of the injection portion a but their combinationQax, with a factor depending on the conditions of the original non-self-slmilarflow whose intermediate asymptotlcs is the self-similar solution of the secondtype (22). It {s essen~al that the {ntermed[ate-asymptofic motion [s notpurely radial in this case. The circumferential component of the velocity forsolution (22) is different from zero, as distinct from solution (16) Thus a, <a ~ the statement of the degenerate problem of a radial source or sinkacting at the vertex of a corner is illegitimate.

3. Finally, if the vertex angle a is exactly equal to the limiting value,a =a,, the intermediate asymptotics is not self-similar at all. As y~0

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SELF-SIMILAR SOLUTIONS 301

Q3 (~’(~)~ In ~d~ ~ In (20cos 2a ~sin20

sin

-- 30 cos 20 + 4 sin 20 -- 50 cos 2a -- 6a0 sin 2a} +o(1)

(23)

so that in this case, too, the statement of the degenerate problem of a radialsource acting at the vertex of a corner is illegitimate.

A similar result has recently been obtained for slow flow of a viscous fluidin a circular cone by Kerchman (1972).

General considerations of self-similar solutions of the first and second type.--The foregoing exainples clarify the matter and make it possible to draw ageneral conclusion.

As is known (Bridgeman 1931, Birkhoff 1960, Sedov 1967), dimensionalanalysis is based on the 1-f theorem, which states that the relation among n + 1dimensional quantities a, al, ¯ ̄ ̄ , a.

a = f(al, ¯ ¯., ak, ak+x, ¯ ¯., a,) (24)

can be represented as

n = F(rh, ¯ ¯., ~,_k) (25)where

aIf= , l-I~= ~ ...,

ala ̄ ̄ ̄ ak" alal ¯ ̄ ̄ aftI(26)

IIn-~ =

It is assumed that the quantities al, . . . , a~ have independent dimensionsand among the quantities al ..... a~ (governing parameters) there exist k-i- 1 quantities with independent dimensions.

The conclusion that a particular governing parameter ak+~ is unimportant(drops out) is usually drawn on the basis of an estimate of the magnitude the corresponding dimensionless parameter 1-/6 The reasoning is as follows:If II~ is "small" or "large" in comparison with unity, the quantity iI~ is re-placed by its limiting value equal to zero or infinity in the expression for thefunction F(H1 ..... II~_~, 171~, II~+~... 1-I~_k), and a function of n--k--1arguments is considered:

~(II1, l’I~, ¯ ̄ ̄ , 17~_~, II~+l, ¯ ̄ ̄ , IL-~)

(27)= F(II1, ̄ " " , 1-1/--1, ~0, 1-[i+1’ . . . , 1-[n--~)

implying that the argument a~+i is unimportant in the problem at hand.

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302 BARENBLATT & ZEL’DOVICH

However, the applicability of this reasoning, as a rule, is based on thetacit assumption that the limit of the function F, when II~ tends to zero orinfinity and the other arguments have fixed finite values, exists and is notequal to zero or infinity. This assumption, however, generally is not ful-filled. In this case the preservation of the governing parameter ak+i is essen-tial, no matter how small or large the corresponding dimensionless para-meter. Of particular importance then is the following special case:

Case 1. The limit of the function F(FI1 ..... II~_l, II~, II~+1 ..... II,_~) II~-~0 or II~--* ~o is zero or infinity, but there is a number a such that the limit

lirn II~-~F = ff(II1, ¯ ̄ ¯ , II~-l, IIi+x, ¯ ̄ ¯ , IIn_k) (28)

as II~--~0 or IIi--~ ~o exists and is not zero or infinity.Further, if the limit of the function F as IIi and IIi tend separately to zero

(for definiteness) exists and is finite, then the sequence and nature of thepassage to the limit are immaterial. If, however, this limit does not exist,then the nature of the limiting process, i.e., the relative rate at which the twoparameters tend to zero, becomes important for the analysis of the asympto-tic behavior. The consideration of both parameters, IIi and 1-Ii, is then essen-tial, no matter how small they may be. Of particular importance here is thefollowing special case:

Case 2. The limit of the function F(II1 .... , II~ ..... IIi ..... II~_~)does not exist but there are numbers a and/3 such that as II~, IIi-*0

(29)Hi+~ ̄ ̄ ¯ II~_~, H~-+~ ¯ ̄ ̄ H._~) -]- ¯ ¯

Of course, it is possible to indicate analogous subclasses in the case ofthree or more dimensionless parameters tending to zero simultaneously.

Consider now a non-self-similar problem for a system of partial differ-ential equations describing a certain phenomenon. The solution of this prob-lem, which is supposed to exist and to be unique, can be represented by(24) and (25) (the functions a are unknown quantities in the problem; quantities a~ ..... a~ are independent variables and parameters of the prob-lem). The self-similar solutions correspond to degenerate problems, which areobtained when some of the parameters II~ tend to zero or infinity, and aresimultaneously the exact special solutions of these degenerate problems witha fewer number of governing parameters and the asymptotic representationsof non-self-similar solutions.

If the limit of the function F exists and is finite, then as a result of theabove-mentioned limiting process self-slmilar solutions of the first type areobtained for which the exponents in the expressions for the self-similar vari-ables are determined from dimensional considerations, using the data of thedegenerate problem as the base. In these problems the pre-self-similar param-eters disappear, leaving no imprint, and can be eliminated from the formu-lation of the limiting degenerate problem.

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SELF-SIMILAR SOLUTIONS 303If no finite limit of the function F exists, then in general there is no solu-

tion of the degenerate problem and the asymptotic representations of thesolution of the non-self-similar problem will not be self-similar for arbitrarilysmall (large) values of dimensionless parameters that are made to approachzero (infinity).

Self-slmilar solutions of the second type owe their existence to the specialcases 1 and 2. This is illustrated by the foregoing examples.

It may happen that the constant A can be found from the integral con-servation laws. This means that it is possible to reformulate the problem and,by suitably choosing the governing parameters, to make the solution of thedegenerate problem a self-similar solution of the first type. For instance, thesolution of the foregoing problem of propagation of strong shock waves canbe obtained as a self-similar solution of the second type if the governingparameter in the pre-self-similar problem is taken, say, not as the energy ofinitial disturbance but as the maximum initial pressure. The possibility ofobtaining the solution of the degenerate problem as a self-similar solution ofthe first type is related to the choice of the governing parameter as the totalenergy E of the initial disturbance which, by virtue of the relevant integralconservation law, is time-independent before the self-similar stage. Anotherexample of this kind is a dipole in the hydrodynamics of an ideal incompres-sible fluid.

~I~ECTRUM OF

We have seen that self-slmilar solutions of the second type are not a rareexception but occur in many problems. In addition to the examples here dis-cussed we must mention the important problem of a converging shock wavestudied by Guderley (1942) as well as by Landau and Stanyukovich (Stanyu-kovich 1955), the problem of short impact considered by yon Weizs~icker(1954) and by one of the present authors (see Zel’dovich & Raizer 1963), problem of collapse of a spherical bubble in an ideal compressible liquidconsidered by Hunter (1960), etc.*

~ The problem of a converging shock wave, in which self-similarity of the secondtype was encountered for the first time, does not obviously admit the use of the lawof conservation of energy for the determination of the exponent. The energy E con-rained in the self-similar region r0 <r <const- r0 tends to zero simultaneously with thefront radius r0 and hence simultaneously with the radius of the self-similar regionand the mass of substance contained in that region. However, E does not decreaseas fast as r0a and consequently the ratio Elm, that is, the energy concentration, andthe wave pressure and other similar quantities tend to infinity. This problem in-volves the principle, specific to gas-dynamic problems, of selection of the exponent~ from the condition relating to a characteristic, i.e., to a line dr/dr=u--c, whichcomes to the center r=O at the same time as the wavefront. For the system of ordi-nary equations to which the system of gas-dynamic equations reduces in a self-similarproblem, this line is transformed into a singular point of the saddle type, which canbe passed through only at the chosen value of the exponent )~. The characteristic atany time is at a distance equal to const.ro from the center; it is precisely this region

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304 BARENBLATT & ZEL’DOVICH

These problems are treated in much detail in Zel’dovich & Raizer (1963)and their analysis from the standpoint of the concepts here developed wouldseem superfluous. We shall focus our attention on the spectrum of elgen-values X and show the connection between the determination of exponentsin self-slmilar solutions of the second type and the classical eigenvalue prob-lem for linear differential operators.

For linear equations such as the classical equations of string vibration orheat conduction, with coefficients depending on the spatial variable but notdepending on time, and subject (for simplicity) to zero conditions at the endsof a finite or an infinite interval, the equations and boundary conditions areinvariant with respect to the group of continuous transformations

u’ = au, t’ = t + ~

(u being the dependent variable). We seek a subgroup of this group andsolutions corresponding to it that convert to themselves under transforma-tions of this subgroup. The subgroup corresponds to a=exp(-~), and thesolutions are of the form

u =Here the X are eigenvalues determined from the condition for existence ofsuch a solution in the large (i.e., satisfying the boundary conditions at theends of the interval) ; they form a set (spectrum) of one structure or another--a spectrum that is discrete, continuous, mixed, etc. We thus arrive at theseparation of variables.

Likewise, the equations and boundary conditions for the uniform-prop-agation regime are invariant with respect to a shift in coordinate and time

x’= x+a, t’= t+~

It is precisely this invarianee that makes it possible to pose the question ofthe existence of a subgroup of this transformation group that leaves thestationary solution u(x, t) invariant, We require that

u(x’, t’) = u(x,

This is possible only when a definite relation exists between the parameters ofthe transformation group, namely when a = --~/3, where X is the eigenvalue of

between the shock wave and the characteristic, ~vhich is not affected from outside,that we term the region of self-similarity. This type of selection is close to the Jouquetrule D = u-[-c in the theory of detonation (see Zel’dovich & Kompaneets 1960).

It should be noted that in a converging wave (but in the linear case where nointersection of the characteristics occurs) there exist self-similar solutions of the firsttype, discovered by Zababakhin & Nechaev (1937); these solutions can be obtainedby superposition of plane waves (Zel’dovich 1937). In this case the existence of solu-tion~ with exponents depending on the initial conditions is revealed (cf footnote 3).

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SELF-SIMILAR SOLUTIONS 305

the problem, which is determined from the condition for existence of thestationary solution

u= U(x + ~t + c)in the large (i.e., satisfying the equations and the boundary conditions atx = _+ oo). In this case, too, the eigenvalues form a set of one structure or an-other. For instance, in the t(olmogorov-Petrovsky-Piskunov problem (1937)the spectrum is continuous (the requirement of stability determines onevalue ?~ =?~0--the lower point of the spectrum) ; in the simplest problem of thetheory of combustion (Zel’dovich & Frank-Kamenetsky 1938) the spectrumconsists of one point, etc.

The situation is quite analogous in self-similar problems. The equationsand the initial and boundary conditions of the corresponding degenerateproblems are invariant with respect to the similarity group. The question isposed as to the existence of a certain nontrivial subgroup of the similaritygroup that leaves solutions of a definite (self-slmilar) type invariant; in thiscase, too, an eigenvalue X naturally occurs, as was shown above.

For self-similar solutions of the first type, the eigenvalues X are foundfrom the conservation laws; in self-similar problems of the second type, theeigenvalue X is determined from the condition for existence of the self-similarsolution in the large. In some cases this condition is sufficient to determineuniquely the eigenvalue. This is the case, for example, in the foregoing modi-fied problem of propagation of strong shock waves for ~/< 2 and 3"~ < 2~/+ 1.In a number of eases, however, the value ~, is not unique; in self-similar prob-lems, too, a continuous spectrum of eigenvalues ), is sometimes obtained.This is the case, for example, in the modified problem of strong shock wavesfor 3’1> 23’ + 1 ; the question of the choice of the eigenvalue is not investigatedhere. The problem of a converging shock wave for 3’>70~---1.87 also furnishesan example of a continuous senfibounded spectrum [see the paper by Brush-linsky & Kazhdan (1963)]. The question of the choice of the eigenvalue re-mains obscure here, though Gel’land’s hypothesis is available (Brushlinsky& Kazhdan 1963), according to which (as in the case of the Kolmogorov-Petrovsky-Piskunov problem) the lower point of the spectrum must in factbe realized. In the presence of a continuous spectrum, however, the values ),that are realized in the self-similar asymptotics may in fact depend on theinitial conditions of the non-self-slmilar problem, whose asymptotics is thisself-slmilar solution of the second type; thus they may in principle be in-determinable from the condition for existence of the self-similar solution ofthe degenerate problem in the large. This is demonstrated by the remarkableresult pertaining to the asymptotics of the solution of the Korteweg-deVries equation obtained by Gardner et al (1957) and by Lax (1968) (see Lick 1970, Kadomtsev & Karpman 1971).

The Korteweg-de Vries equation, which describes plane waves in shallowwater, has the form

O,u + uO~u + flO~*u = O, fl = coh~/6, co = ~/gh (30)

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306 BARENBLATT & ZEL’DOVICH

FIGUP~ 3. The soliton.

where g is the acceleration of gravity and h the depth of the undisturbedlayer of fluid. This equation has solutions of the type of uniformly propagat-ing waves

u = u(¢) = uoch-2[ / o/l@ (31)where

~ = x-- Vt-c, V= Uo/3 (32)

and t is the time, x the axis of abscissas of a system moving relative to thefluid with velocity co-t-u~, and u~ the velocity at infinity. These are the so-called solitary waves or "solitons" (Figure 3). The result obtained in Gardneret al (1967) and Lax (1968) is, that for t--* ~o and large positive values of the solu~on of the inltlal-value problem with a su~clently rapidly decreasinginitial distribution u(x, 0) is represented as a sequence of solitary waves(Figure 4) moving in the positive direction with velocities proportional their amplitudes

It is fortunate that the X~ coincide with the discrete elgenvalues of theSchr~dinger operator

~, + ~ iX + u(x, 0)]~ = 0 (34)

so that the "inverted" initial distribution plays the role of the potential here.We now change the variables

x= ln~, t = lnr, c,~ lnA~

The Korteweg-de Vfies equation is then rewritten as

.O.u + ~uO~u + O(~"~,~du + 3~o~du + ~o,u) = 0 (35)

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SELF-SIMILAR SOLUTIONS

FIGURE 4. The initial disturbance at t-~ oo and large x givesrise to a sequence of solitary waves.

307

and the asymptotics (33) takes a very simple self-similar form

{ ’F- 1(36)

,1--,Thus the initial distribution determines N constants, A~, . . . , A~ withvarious transcendental dimensions and N intervals in ~ such that, as r~ ~,~ = 0(r~1~1/~) within each interval; and in each of these intervals the asympto-tics of the solutlon of the Cauchy problem is of the form

l E ~

(The contribution of the other terms i~ this interval is obvlou~ly negligible.)The foregoing example shows that in the case of a continuous spectrum

the exponent ~, like the constant A, can be determined by the initial ¢ondi-tio. of the non-self-slmilar problem so that the system can "remember" notthe amplitude or the wi4th of the initial dlstrubance but, in general, a numberof their ¢ombina~ons with various dimensions; in this case not only themagnitudes but also the dimensions oi the constants remembered by theintermediate asymptofics depend on the initial condition and mu~t be deter-mined by following (~ay, numerically) the evolution of the non-self-slmilarsolution. It remains to be seen what is the situation in the case of a converg-ing shock wave for V>~o~l.87--whether it is as suggested by Gel’land oras described above or something else.

In addison to the solu~on oi the "sollton" type the Korteweg-de Vrlesequa~on has a set of stationary solutions periodic in ~ of the form

u(t) = ~ * --, s (38)

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308 BARENBLATT & ZEL’DOVICH

where dn is Jacobi’s elliptic function of modulus s and a is the amplitude ofvibration; the wavelength A, the average value ~, and the velocity V areexpressed by the formulas

A = 2sK(s)V~--’ f~ ~ K-s’’() V --3s 2 = m (39)

where K(s) and E(s) are elliptic integrals. Putting again x ~ In ~, c ~ In A, andt ~ In r, we obtain the self-similar solution of Equation (35)

u = ~ dn* ~ In ~, s (40)

which periodically reproduces itself (on a variable scale). A very elegantidea concerning periodic self-similarities is due to Zababakhln (1965, 1970).Studying the propagation of shock waves in a continuous medium withperiodically distributed properties, Zababakhin constructed a solution thatalso periodically reproduced itself on a variable scale. To construct thesolution, he followed the evolution of the initial impulse by numerical cal-culation.

Mo~ G~a~ Gaouvs

The ~elf-similarity of a particular intermediate agympto~c8 may berelated to the invaria~ce of ~he stateme~t of the degenerate problem withrespec~ to a more general transformation group than the group of similaritytransformations of quanti~es with independent dimensions.

Precise general formula~ons concerning the relationship between in-variance (symmetry) and self-similarity, a~ well a~ reference~ to some earlierworks that advance such assertions and treat ~pecial examples, are containedin the well-known book of Birkhoff (1960). Therefore we restrict ourselves several illu8tm~ve examples.

The simplest example is the Blasius solu~on of the equa~ons of theboundary-layer theory. We sh~ll coasider it since the method of reducing tothe formal procedure of dimensional analysis as here applied is a typical oneand is useful in many other problems. The corresponding degenerate problemis of the form (the nota~on is standard)

u O~u + v O~u = v Out’u, O~u + Ou~ ~ 0(~)

~(o, ~) ~(~, ~)= v, ~(~, o) = ~(~, o) The use of dimensional considerations in the usual way is insu~cient to

prove the self-slmilarlty of the solution of the degenerate problem (41).[That is, the quantity u depends on the variable and constant parametersx, y, U, and v, only two of which have independent dimensions, so thatdimensional analysis gives u=f(y/x, y/~.] Inspectional analysis (inthe general formula~on of Birkhoff 1960) shows, howeve¢, that the proble~

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SELF-SIMILAR SOLUTIONS 309

(41) is invarlant with respect to a three-parameter group of similarity trans-formations, and not just to the two-parameter group that follows from simpledimensional analysis. This may be expressed in an alternate form: In thisproblem the variables x and y may be regarded as having different dimen-sions L~ and L~; this is formally possible because of the neglect of the term v0~x~u on the right-hand side of the first equation of (41) in comparison withthe corresponding Navier-Stokes equation. Then for the terms in each of therelations (41) to have the same dimensions, we must take the dimensions the quantities appearing in (41) to be the following:

[u] = v, iv] = VL, L,-1, = (42)Applying now the conventional technique of dimensional analysis (thegoverning parameters being U, v, x, and y, the dimensions of the first three ofwhich are independent), we obtain the representation of the solution inaccordance with the H theorem in the form

u = UfU: ’ v =

ixU: (43)

that is, we have proved that the solution to the degenerate problem is in-dependent of the argument y/x.

Another illustrative example of self-similarity due to the invariance of thestatement of the degenerate problem with respect to a more general trans-formation group than the group of similaNty transformations of quantitieswith independent dimensions is furnished by so-called "limiting" self-similarsolutions, i.e., solutions of the form e~(x~), which have long been pointedout in boundary-layer theory by Goldstein (1939) and in gas dynamics Stanyukovieh (1945).

We demonstrate the proof of self-similarity of these solutions based onthe invafianee of statements of degenerate problems with respect to moregeneral transformation groups by considering a simple problem of nonlinearfiltration theory (Barenblatt 1954). The statement of the degenerate problemis, in this case (where p=p(x, t)is the gas pressure for x~0 and t> - ~),

O,p = KOz~2p2, p(x, -- ~ ) = O, p(O, t) = poe** (44)

Dimensional analysis (the H theorem) shows only that the solution of theproblem can be written as

~ = ~oF(X/V~-~o, .t) (4~)We now observe that the statement of the problem i~ invariant with

respect to a ~hift in time. If we t~ke #=¢~+~, where ~ i~ an arbitrary con-~tant, the equation and the first two conditions of (44) remain unchangedand the third condition of (44) assumes the form p(O, t’)=p’oe ~(, wherep%=poe~. Thus, the time shift reduces to a similarity transformation of P0only. According to (45) we have

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310 BARENBLATT & ZEL’DOVICH

p(x, t’) = po’F(z/V’Kpo’ -x, at’)(46)

= poe°"F(x/’C’~po’a-1, at --

from which it follows that the function F(~, ~) satisfies the relation

F(~, ~) = e~’F(~e-~/~, ~ -- ~) (47)

Putting now r =~/a=t, we find F(~, ~) =e’F(~~/~, 0) =e~(~"/~), and thistogether with (45) then gives the self-similarity of the solution of the de-generate problem (44)

p = poe~¢(x/~poe~’~-x ) (48)

The solution (48) is the limit, as a~0 and the initial time tends suitablyto -~, of self-similar solutions of the ordinary power-law type (t--to)~

f(x/(t--to)a), for which the degenerate problem i~ of the form

O,p = ~O,,~p ~, p(x, to) ~ O, p(O, t) = u(t -- ~ (49

An illustrative example of self-similar problems for which self-similarityis related to the invariance of the statement of a problem with respect to amore general transformation group than the group of similarity transforma-tions of quantities with independent dimensions is provided by the well-known problem of Sobolev (1954) concerning the stability of rotation of incompressible fluid in a cylindrleal vessel. The equation for the pressuredisturbance in this problem is of the form

1a.~Ap + ~ a..~p = O, A = a~~ + ~ a. + a..~ (50)

where 0= ~x~+y~, ~ is the angular velocity of rotation, and the g axis isdirected along the angular velocity.

As shown by Sobolev, the fundamental solution of this equation is self-similar and is written as

po(X, y, z, t) = -- (Sl)

where r = ~o~+z~ and ~ (~) =fo~Yo(~)d~, and it is clear that its self-similaritycannot be established from dimensional considerations alone (the quantitieswt and o/r are both dimensionless); the corresponding additional group isfound in a way similar to that used above.

The foregoing examples demonstrate the importance of the idea of thegeneralized inspectional analysis of Birkhoff in establishing the self-similarltyof intermediate asymptofics. Naturally the question arises as to the deter-mination of all groups of continuous transformations under which a givensystem of partial differential equations is invariant. The relevant generalresults, which develop the fundamental ideas of Lie, have recently been ob-

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SELF-SIMILAR SOLUTIONS 311

rained by Ovsyannikov (1962). He and his collaborators applied these generalresults to the analysis of a number of specific equations.

In the present review an attempt is made to take a somewhat differentlook at self-slmilar solutions and primarily to show their role as intermediateasymptotics. We have endeavored to clarify the nature of the difference be-tween self-similar solutions of the first and second type and to demonstratean intimate connection existing between self-similar solutions, uniform

propagation regimes, and elgenvalue problems.We are grateful to R. V. Gol’dshtein and V. I. Kerchman for useful dis-

cussion of the work.

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