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Experimental and Numerical Investigation of a Single Loop Pulsating Heat Pipe 8 th semester project work by IDUL AZHARUL HOQUE (Roll Number: SC11B029) Department of Aerospace Indian Institute of Space Science and Technology Thiruvananthapuram April 2015

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Page 1: pulsating heat pipe report

Experimental and Numerical Investigation of a Single Loop

Pulsating Heat Pipe

8th semester project work

by

IDUL AZHARUL HOQUE

(Roll Number: SC11B029)

Department of Aerospace

Indian Institute of Space Science and Technology

Thiruvananthapuram

April 2015

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BONAFIDE CERTIFICATE

This is to certify that this project report entitled Experimental and Numerical

Investigation of a Single Loop Pulsating Heat Pipe submitted to Indian

Institute of Space Science and Technology, Thiruvananthapuram, is a bonafide

record of work done by IDUL AZHARUL HOQUE under my supervision from

10/01/2015 to 20/04/2015.

Dr. Pradeep Kumar P

Dr. A. Salih

Head of Department

Aerospace Engineering, IIST

Place:

Date:

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Declaration by Author

This is to declare that this report has been written by me. No part of the report is

plagiarized from other sources. All information included from other sources have

been duly acknowledged. I aver that if any part of the report is found to be

plagiarized, I shall take full responsibility for it.

Md. Idul Azharul Hoque

SC11B029

Place:

Date:

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Contents

Acknowledgement............................................................................................................................I

Abstract........................................................................................................................................... II

Nomenclature................................................................................................................................. III

List of figures...................................................................................................................................V

Chapter 1: Introduction.........................................................................................................................1

1.1 Nature of a PHP...........................................................................................................................1

1.2 Objective of the work..................................................................................................................4

1.3 Organization of the report...........................................................................................................5

Chapter 2: Literature Survey.................................................................................................................7

2.1 History.........................................................................................................................................7

2.2 Review of studies conducted on pulsating heat pipes.................................................................9

2.2.1 Experimental studies:..........................................................................................................9

2.2.2 Numerical studies..............................................................................................................13

2.3 Inference....................................................................................................................................15

Chapter 3: Numerical Modelling..........................................................................................................16

3.1 Reference frame........................................................................................................................17

3.2 Forces acting on the liquid slug and equation of motion:..........................................................17

3.3 Energy equation of the vapor plugs...........................................................................................19

3.4 Mass balance at the interfaces..................................................................................................20

3.5 Energy equation of liquid slug:..................................................................................................21

3.6 Numerical solution:....................................................................................................................24

Chapter 4: Experiment.........................................................................................................................28

4.1 Experimental Setup....................................................................................................................28

I

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4.2 Properties and dimensions of parts used:.................................................................................29

4.3 Procedure..................................................................................................................................34

4.4 Results.......................................................................................................................................35

4.5 Probability of errors:..................................................................................................................36

Chapter 5: Results and Discussion.......................................................................................................38

5.1 Theoretical results:....................................................................................................................38

5.2 Experimental results..................................................................................................................43

5.2.1 40% filling ratio:.................................................................................................................43

Chapter 6: Conclusion.........................................................................................................................44

Appendix........................................................................................................................................45

References.................................................................................................................................................46

II

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Acknowledgement

I thank with gratitude for the guidance, suggestions and encouragement forwarded by several

respected persons and I know well that it is impossible to express my indebtedness for all those

valuable assistances in this finite piece of paper. I acknowledge in this page, the assistance

rendered by all the concerned persons, as a token of my gratitude. I am feeling honored to

express my sincere appreciation and deep gratitude to Dr. Pradeep Kumar P for his supervising

throughout the internship, for his valuable guidance, friendly encouragement and helping me to

acquire substantial knowledge in preparing whole process layout and experimental work. Entire

work has been carried out in the Manufacturing Lab and Heat and Thermal Lab of IIST,

Thiruvananthapuram. I would like to convey my thankfulness to the lab assistants Bipin Sir and

Dinesh Sir for their help without which I would have never been finish my project.

Md. Idul Azharul Hoque

SC11B029

I

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Abstract

The oscillatory motion of the pulsating heat pipe (PHP) is highly non-linear. The objective of this project was to study the behavior of a typical closed PHP with a theoretical model based on Ma and Qu’s work and experimentally determine the temperature and pressure values in a closed PHP. A mathematical model is described and a MATLAB program is run to find the numerical solution. The results are compared with the source paper. Thermocouples and pressure transducer is used to find the temperature and pressure at various location in our experimental setup. The effect of filling ratio and inclination angle is experimentally determined. We compared the experimental results and theoretical results by finding the initial conditions in the experiment and incorporating it in our MATLAB program.

Key Words: PHP, latent heat, sensible heat, evaporator, condenser

II

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Nomenclature

Bo Bond Number.

c pv Specific heat of the vapour at constant pressure [J/KgK]

cvv Specific heat of the vapour at constant volume [J/KgK]

d Internal diameter [m]

Ac Cross sectional area [m2]

σ Surface tension [N/m]

ρl iq Density of liquid [kg/m3]

g Acceleration due to gravity [m/s2]

Lp Length of liquid plug [m]

Lh Length of the pipe in the heater region [m]

Lad Adiabatic length [m]

Lc Length of the pipe in the condenser region [m]

x p Position of the vapor bubble [m]

h fg Latent heat of vaporization [J/kg]

T e Temperature of the heater [K]

T v Temperature of vapor plug [K]

T c Temperature of condenser [K]

ṁ Mass transfer rate [kg/s]

mv Mass of vapor plug [kg]

m p Mass of liquid plug [kg]

III

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he Overall heat transfer coefficient for heater region [W/m2˚C]

hc Overall heat transfer coefficient for condenser region [W/m2˚C]

C f Co-efficient of friction

Re Reynolds’s Number

μl Viscosity of liquid [Kg/m sec]

Pe External Pressure [Pa]

Pv Pressure of the vapour bubble [Pa]

iv Specific enthalpy [J/KgK]

IV

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List of figures

Figure 1-1: (A) Typical PHP (B) Open loop PHP (C) Closed loop PHP..........................................................................2

Figure 2-1: Dunking Bird.............................................................................................................................................4

Figure 2-2: Loop type heat pipe [Akachi, 1990].........................................................................................................6

Figure 3-1: A multi-turn CLPHP with symmetrical distribution of liquid and vapor..................................................8

Figure 3-2: Single liquid slug and two adjacent vapor plug model with co-ordinate frame.....................................9

Figure 3-3: Vapor plugs at xp<0............................................................................................................................13

Figure 3-4: Vapor plugs at xp≥ 0............................................................................................................................13

Figure 3-5: Conduction and convection relating to the liquid slug..........................................................................14

Figure 4-1: Pressure cooker as evaporator...............................................................................................................20

Figure 4-2: Copper tube shape and dimensions.......................................................................................................21

Figure 4-3: Glass tube dimension.............................................................................................................................22

Figure 4-4: Condenser box made of acrylic plates...................................................................................................22

Figure 4-5: Setup to change the angle of inclination...............................................................................................23

Figure 4-6: Final assembly........................................................................................................................................25

Figure 4-4-7: (1) Data base system (2) Ice junction (3) Complete setup (4) voltage distributor.............................26

V

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Chapter 1: Introduction

Modern world is gripped by machines and electronics. Every machines or electronic

device gets heated due to the high heat density. Each upcoming nano-design is with

higher power dissipation and higher heat density. Pulsating Heat Pipes (PHPs),

characterized by highly effective evaporation and condensation cycles offer an

effective heat remover greater than the traditional ways. PHPs do not require

mechanical pumps or valves or consume any power and also quieter and reliable.

1.1 Nature of a PHP

A PHP consists of a metallic tube of capillary dimensions bend in serpentine

manner and joined end to end (closed loop) or open end (open loop) .These structures

are characterized by the given basic features:

(a) The structure is made of meandering tube of small capillary dimensions with

turns .This tube can be either:

Open Loop: tube ends are not connected to each other.

Closed Loop: tube ends connected to each other.

(b) There is no internal wick structure.

(c) At least one heat receiving (heater) region is present.

(d) At least one heat dissipating (condenser) region is present.

A PHP is essentially a non-equilibrium heat transfer device driven by complex

combination of various types of two-phase flow instabilities. The construction of the

device inherently ensures that no external mechanical power source is needed for the

fluid transport. The driving pulsations are fully thermally driven.

1

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Figure 1-1: (A) Typical PHP (B) Open loop PHP (C) Closed loop PHP (1)

The parameters that influences the overall performance and dynamics of the PHP

are:

1. Tube diameter:

The flow mode is ‘pulsating’ only under certain range of diameters. Bond number (or

Eötvös) criterion (2) gives the design rule for diameter

(Eö)crit=(Bo)crit2=

dcrit2 . g .( ρliq− ρvap)

σ≅ 4

∴ dcrit=2×√ σg .(ρliq−ρ vap)

This criteria ensures that plug flow (figure1-2) is exhibited and they do not

agglomerate leading to stratified phase separated flow (figure1-3).

For d<dcrit there will be a plug flow resulting in pulsation. But it can’t be so

small because for a given specified heat power, decreasing the diameter will increase

the dissipative losses and lead to poor performance.

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Figure 1-2: Plug flow (1)

As the diameter increases beyond dcrit ,the surface tension is reduced and all the

working fluid tend to stratify by gravity and the pipe will stop functioning as a PHP

rather it will operate as interconnected array of two-phase thermosyphons.

Figure 1-3: Stratified flow (1)

2. Filling ratio (3):

Filling ratio is the fraction (by volume) of the heat pipe which is initially filled with

the liquid. Experimental results so far indicate that there is an optimum filling ratio

for proper PHP operation (in the pulsating mode of operation). This optimum,

however, is not sharply defined but generally is around 40% - 70% fill charge.

A too high filling ratio above the optimum leads to a decrease in the overall

degree of freedom as there are not enough bubbles for liquid pumping. At 100%

filling ratio, the device acts as a single phase buoyancy driven thermosyphon. In this

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mode too, substantial heat transfer can take place, but the action is limited to bottom

heat mode only.

3. Heat Flux (2):

The applied heat flux affects the following:

(a) Internal bubble dynamics, sizes and agglomeration,

(b) Level of perturbations and flow instabilities , and

(c) Flow pattern.

PHPs are inherently suitable for high heat flux operation. Since the input heat

provides the pumping power, below a certain level, no oscillations commence. In

case of CLPHPs, a unidirectional circulating flow has been observed at high heat

fluxes.

4. Number of turns (2):

The number of turns increases the level of perturbations inside the device. If the

number of turns is less than a critical value, then there is a possibility of a stop-over

phenomenon to occur. In such a condition, all the evaporator U-sections have a vapor

bubble and the rest of the PHP has liquid. This condition essentially leads to a dry out

and small perturbations cannot amplify to make the system operate self-sustained.

If the total heat throughput is defined, increasing the number of turns leads to a

decrease in heat flux handled per turn. Thus, an optimum number of turns exits for a

given heat throughput.

Other parameters which too affect the operation are

Working fluid thermal properties.

Device orientation.

Tube material thermal characteristics.

4

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1.2 Objective of the work

The dynamics and working of a PHP is very complex and highly non-linear.

Although there are many studies conducted on PHPs, the mechanism of fluid flow

and heat transfer of PHPs is not well understood. Many authors have tried to reason

the behavior of the dynamics of the PHP but is not able to converge to a definite

solution. Questions have been raised if gravity have any effect on the pulsation mode

of heat transfer, what is the contribution of latent and sensible heat on the total heat

transfer amount, how the filling ratio effects the pulsation mode, how the boundary

conditions effect the temperature distribution and heat transfer rate, etc. Many authors

have different answers to the questions. We tried to validate and understand the

reasoning by doing and experiment based on one of various models forwarded and

compare the results to validate the theory or find out errors and to have a better

understanding of the dynamics of a PHP.

A mathematical model is made based on previous studies. Some assumptions

and symmetrical behavior is considered to simplify the model. A MATLAB program

is executed to find out numerical solution of the equations based on the model. The

results are analyzed and compared to the previous model’s results and effects of

various physical parameters are evaluated from the results.

An experiment is conducted based on the model and the results are analyzed

and compared with our theoretical results. Experimental results for different

conditions are extracted and analyzed.

1.3 Organization of the report

The report contains a substantial amount of previous studies both numerical and

experimental on PHP. We did a survey of these previous literature and compared the

inferred the differences among them and took a model among them for our study. We

made a theoretical model based on Qu & Ma’s paper ‘Flow and heat transfer of liquid

plug and neighboring vapor slugs in a pulsating heat pipe’ [2009] and wrote a

MATLAB code to solve the equations derived numerically, Effect of different

5

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parameters like inclination, temperature gradient and initial conditions were seen. The

aim for the experiment is discussed after the model. Parts, assemblies, procedure and

results of our experiment is broadly discussed. Then in our result and discussion

section the results from both the modelling and experiment. The results from our

program were analyzed and compared with the paper’s result. The experimental

results were compared with our experimental results with the same given conditions.

The need of PHP, our study and understanding and the future works related are also

discussed in the conclusion section. Appendix contains the MATLAB code,

thermocouple calibration sheet, experimental temperature sheet from data acquisition

system and derivation of the equations in our model.

6

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Chapter 2: Literature Survey

2.1 History

‘Drinking’ or ‘dunking duck’ (1), a popular toy may be the vital link in the

evolutionary of the modern PHPs. The bird’s body is made up of a glass tube with

two bulb like container on both ends (head and tail). The device is partially filled with

volatile working fluid (having boiling point around 40˚C). When the bird is upright

the vapor in the head doesn’t connect with that in the tail section as seen in the

figure2-1. The evaporation hence mass transfer from the head end generates a low

vapor pressure inside hence the working fluid is pushed up in the neck rising the

centre of gravity.

Figure 2-4: Dunking Bird (1)

A time comes when the mouth end weighs more than the tail and the duck’s head

goes down and touches the water beaker and re-wet the fuzzy cloth attached to the

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beak. In this horizontal position, the two vapor pockets are connected so that the

liquid in the body can freely move. All the liquid is pulled back by gravity to the tail

container and again the evaporation from beak will cause pressure difference and the

cycle continues.

While it is difficult to trace the origin of the ‘drinking duck ’, another

presentation of an analogous concept is found in a patent filed in the former

USSR ,Smyronv and Savchenkov, 1975 (1). It consists of an evaporator and a

condenser bulb connected by a tube. At first evaporator end bulb of the connecting

tube is completely filled by a working fluid while the condenser bulb is partially

filled and the rest is filled by some passive gas.

Figure 2-5: Details of the patent shown by Smyronv and Savchenkov (1)

Heating at the evaporator expands the working fluid and pushes it to the condenser.

Further heating generates vapor in the evaporator bulb and pushes the liquid further

and hence compressing the trapped passive gas. The passive gas is substantially

compressed at this stage. The potential energy stored in the passive gas at some stage

push back the liquid back to the evaporator and the cycle continues.

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With this brief introduction we shall now review the modern PHP studies and

experiment conducted.

2.2 Review of studies conducted on pulsating heat pipes

Pulsating Heat Pipes, after their development in the early 90s, have been actively

employed in thermal management of microelectronics. Although a variety of designs

are in use, understanding of the fundamental processes and parameters affecting the

PHP operation are still vague. Experimental and numerical analyses of such flows

require more stringent time and spatial resolutions and hence there exists fewer

investigations of pulsating heat pipe. As the need of effective and efficient heat

removal mechanism is increasing with the sophistication in electronics and other

nano-designs the attention towards the PHP’s realization and use is increasing.

2.2.1 Experimental studies:

Although the basic idea of PHP is in the patent presented by Smyronv and

Savchenkovn [1975] the exploitation of the concept of PHP from an engineering

point of view was done by Hisateru Akachi in 1990. In this patent, the inventor

disclosed twenty four different preferred embodiments of what is referred to as Loop

Type Heat Pipe. While the fundamental aspects common to all the embodiments are

similar to the PHPs, these proposed structures are essentially characterized by the

presence of at least one non return flow control check valve integrated in the tubes for

imposing a preferred flow direction. The typical tube cross sections employed were

2.0mm or more, always ensuring that the diameter is below a prescribed limit for

liquid and vapor phases to form distinct plugs due to surface tension effects. All the

proposed structures were characterized by the presence of at least one non-return flow

check valve for imposing a preferred flow direction.

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Figure 2-6: Loop type heat pipe and its different designs (1)

Figure 2-7: PHP’s as designed by Akachi (1)

Many works on PHP was done based on Akachi’s concept. C Wilson and his group

conducted a visual and thermal experimental investigation of four pulsating heat

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pipes (PHPs) to observe fluid flow of liquid plugs and vapor bubbles in the PHP and

its effect on the temperature distribution and heat transfer performance in a PHP (4).

Four PHPs were constructed for this experiment, two open loop Figure 2-5(A) and

two closed loop PHPs Figure 2-5(B).

Figure 2-8: Wilson’s OHP prototypes: (A) schematic of the open loop OHP,

(B) Schematic of the closed loop OHP, (C) photo of the finished

OHP, and (D) neutron radiography image of the OHP (4)

The heat pipes were charged with high performance liquid chromatography (HPLC)

grade water or HPLC grade acetone at different filling ratios. Each OHP was

instrumented with 24 T-type calibrated thermocouples. Figure 2-7 illustrates the

temperature variations between the water PHP and acetone PHP including the effects

of orientation and loop type at a condenser temperature of 20°C and a power of 100

W.

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Figure 2-9: Evaporator temperature oscillations at 100 W and a condenser

temperature of 20°C: (A) water OHP and, (B) Acetone PHP (4)

They experimentally found the effects of the temperature gradient, fluid properties

and orientation in the heat transfer rate and the amount of heat transfer.

Robert Thomson Dobson conducted an experiment on open loop PHP based on his

own theoretical model on open loop PHP. He made a comparison of the temperature

distribution and pressure force of both his theoretical modelling and experimental

result to validate his theory.

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Figure 2-10: Dobson’s comparison of theoretical and experimental result (5)

Many other experiments have been conducted recently to understand how a PHP

behaves and to find out effects of various physical parameters.

2.2.2 Numerical studies

Robert Thomson Dobson forwarded a theoretical model on open loop PHP. His

famous Dobson boat model describes how an open PHP mechanism works in a ‘putt

putt’ boat (6).

Figure 2-11: ‘putt putt’ boat (an open PHP) (6)

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Theoretical results of his model includes the liquid plug velocity, position and the

thrust due to pressure difference resulting the motion of the boat with respect to time.

He also conducted an experiment to validate his theory.

Figure 2-12: Dobson’s theoretically determined thrust as a function of time (6)

Dazhong Yuan, Wei Qu and Tongze Ma also proposed a theoretical model on closed

loop PHP. They studied previous works on PHP and found the difference in the views

of different authors. In their work they pointed out how gravity effects the behavior

of PHP and its heat transfer capabilities. They also found the fraction of heat transfer

by sensible and latent heat (7). In their model some assumptions were made to

simplify the problem. Their results included the temperature, pressure and position

variation inside the PHP and the amount of heat transfer by sensible and latent heat

and their response to the initial conditions and gravity.

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Figure 2-13: Comparison of sensible heat replaced by latent heat by Ma and

group with previous Zhang’s work (7)

2.3 Inference

From the above discussion of the works done on PHP we can easily see the objective

of the works and the differences in the results. In the experiments it is tried to validate

the theories proposed on the mechanism and behavior of a PHP. New theories are

developed and experimental data has to be compared to validate the same. Studying

various models and experiments we decided to study Ma and Qu’s model and do a

MATLAB program to find numerical solution of the equations based on is model.

Validation of his model by experimental data is not yet done and we conducted an

experiment to validate his theory. We also conducted experiment to study the effects

of filing ratio and gravity and fluid thermal properties.

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Chapter 3: Numerical Modelling

A closed loop pulsating heat pipe (CLPHP) contains one or more loop closed in both

ends. Based on Ma and Qu’s study a model is made on closed loop pulsating heat

pipe. It is assumed that fluid is symmetrically distributed into liquid and vapor inside

the pipe and our model considers a part consisting only one liquid slug between two

vapor plugs as shown in Figure 3-1.

Figure 3-14: A multi-turn CLPHP with symmetrical distribution of liquid and

vapor

Some assumptions are made such as:

1 The vapor plugs in two evaporators observe the ideal gas law.

2 The mass and energy exchanges occurred on the interface between the vapor

plugs and the liquid slug are due to the phase change.

3 The shear stress on the tube wall is related to the fluid flow state.

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3.1 Reference frame

A one-dimensional coordinates with the right direction as the positive is set up along

the tube. The origin of the coordinates is set at the right intersection of the heater and

the condenser. The liquid slug is assumed as a particle, the displacement of which is

the displacement of the right end of the liquid slug form the origin.

Figure 3-15: Single liquid slug and two adjacent vapor plug model with co-ordinate frame

3.2 Forces acting on the liquid slug and equation of motion:

When x p is positive i.e. liquid plug moves up in the right side gravity force of 2 x p

length of liquid acts downward i.e. in the negative direction. Therefore the

gravitational force acting is:

Fgravity=−ρL Ac (2 x p) g

The driving force is the pressure difference of the two vapor plugs acting on the

liquid slug. Therefore the driving force is:

F pressure=(P¿¿ v1−Pv 2) Ac¿

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The motion of a vibrating particle is restrained by the wall shear stress which is a

damping force:

F friction=−πd Lp τ p

Where shear stress is proportional to the velocity as:τ p=12

Cρ( dxdt

)2

Where C is called the viscous coefficient and dependent on the flow state (laminar,

transition and turbulent), or on the Reynolds number .We adopted Swami and Jain’s

explicit co-relation accounting for the surface roughness as:

C=14

¿¿

F friction=−πd Lp12

ρL C (d x p

dt)

2

Hence we have our pressure force and one friction force and one gravitational force

acting on the liquid slug during its motion. Hence by newton’s law our equation of

motion is:

Lp Ac ρL

d2 x p

d t 2 =(P ¿¿v 1−Pv 2) Ac− ρL Ac(2 x p)g−πd Lp12

C ρL (d x p

dt)

2

¿

Rearranging we get[APPENDIX]

d2 x p

d t 2 + 2 Cd

(d xp

dt)

2

+ 2gLp

x p=(P¿¿ v1−Pv 2)

Lp ρL

¿

The equation is similar to the governing equation for forced damped mechanical

vibrations. It is a second-order nonlinear differential equation. The damping force

term 2Cd

changes with the flow velocity.

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3.3 Energy equation of the vapor plugs

We consider the heat input or output to the vapor plugs due to phase change. Our

general heat equation is:

dHdt

= pdvdt

+ dqdt

For the 1st vapor plug (left side) as it is compressing the liquid slug i.e. work is done

by the vapor plug we have our energy equation as:

d mv1 cv T v 1

dt=−Pv 1

d Ac xp

dt+

d mv1 hfg

dt

Simplifying we get:

mv 1 cv

d T v 1

dt+cv T v 1

d mv 1

dt=−Pv 1 Ac

d x p

dt+

d mv 1

dth fg

For the 2nd vapor plug (right side) as it is being compressed i.e. work is done on the

vapor plug we have our energy equation as:

d mv2 cv T v2

dt=Pv 2

d Ac xp

dt+

d mv2 hfg

dt

Simplifying we get:

mv 2 cv

d T v2

dt+cv T v 2

d mv 2

dt=Pv 2 Ac

d x p

dt+

d mv 2

dth fg

As we have assumed the vapor as ideal gas we can write:

For the 1st plug

Pv 1(Lh+x p) Ac=mv1 R T v1

Differentiating with respect to time we get:

(Lh+x p) Ac

d Pv 1

dt+Pv 1 Ac

d x p

dt=mv 1 R

d T v 1

dt+R T v 1

d mv 1

dt

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And for the 2nd plug

Pv 2(Lh−x p) Ac=mv 2 R T v 2

Differentiating we get:

( Lh−x p ) Ac

d Pv2

dt−Pv 2 Ac

d xp

dt=mv2 R

d T v 2

dt+R T v 2

d mv2

dt

3.4 Mass balance at the interfaces

The mass change of the vapor plugs is related with the evaporation and/or

condensation processes. We assumed that this change occurred only at the interfaces.

Therefore the mass of the vapor plugs will change according to mass flux equation:

m' '= q ' '

h fg

=U (Th , c−T v)

h fg

For the 1st vapor:

d mv1

dt={ −hc πd x p(T v 1−T c)

h fg

,∧x p≥ 0

he πd (Lh+ xp)(T e−T v 1)hfg

,∧x p<0

For the 2nd vapor:

d mv2

dt={he πd

(Lh−x¿¿ p)(Te−T v 2)hfg

,∧x p ≥0¿hc πd x p(T v2−Tc )

hfg

,∧x p<0

20

O

For positive x

O

For negative x

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3.5 Energy equation of liquid slug:

To find the temperature distribution within the liquid slug with respect to time and

space we have to build another equation. The energy input/output to/from the liquid

slug will give the energy hence temperature distribution. The heat transfer to/from the

liquid plug is the sensitive heat transfer. Both conduction and convection is occurring.

Conduction is from the adjacent vapor plugs and convection to the outside or

environment.

Figure 3-18: Conduction and convection relating to the liquid slug

Conduction equation:

AC

∂(K∂T∂ x

)

∂ x=AC ρ c p

∂ T∂t

Convection equation:

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−hliq A (T−T wi)=AC ρ c p∂ T∂t

Note that the co-ordinate frame here is different from the previous frame. The new

frame of reference is having origin at the intersection of heater and condenser:

Figure 3-19: Co-ordinate frame for the energy equation of liquid slug

Hence our energy equation of the liquid slug is:

ρ c p AC∂ T∂t

=AC

∂(K∂ T∂ x

)

∂ x−hliq A (T−T wi)/ AC

As T wi is not known we can extend to the environment temperature T ∞ by

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ρ c p∂ T∂ t

=∂ (K

∂ T∂ x

)

∂ x−

4 Ud AC

(T−T ∞)

Where,

1U

= 1hliq

+d i

d0h∞

+ Kt

The initial and boundary conditions are:

T ( x=0 ,t )=T v 1

T ( x=LP , t )=T v2

T ( x , t=0 )=T ∞

And the variation of the outside temperature is:

T ∞={ T c ,∧0<x<Lc

T e ,∧x>Lc , x<0

Once the results of the temperature distribution are obtained, the sensible heat is

calculated. The heat input to the liquid slug from outside is:

Q¿ ,liq=∫x¿0

x¿Lp

πdK (T ∞−T )dx ,T ≤T ∞

And heat output from the liquid slug to outside is:

Qout , liq=∫x¿ 0

x¿Lp

πdK (T−T∞)dx ,T ≥ T ∞

Hence total heat transfer is both due to the latent heat transfer in vapor and sensible

heat transfer in the liquid slug.

Qtotal ,∈¿=Q ¿ , liq+Q¿ ,vap ¿

Qtotal , out=Qout ,liq+Qout , vap

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3.6 Numerical solution:

So we have our equations as:

d2 x p

d t 2 + 2 Cd

(d xp

dt)

2

+ 2gLp

x p=(P¿¿ v1−Pv 2)

Lp ρL

¿

mv 1 cv

d T v 1

dt+cv T v 1

d mv 1

dt=−Pv 1 Ac

d x p

dt+

d mv 1

dth fg

mv 2 cv

d T v2

dt+cv T v 2

d mv 2

dt=Pv 2 Ac

d x p

dt+

d mv 2

dth fg

Pv 1(Lh+x p) Ac=mv1 R T v1

Pv 2(Lh−x p) Ac=mv 2 R T v 2

d mv1

dt={ −hc πd x p(T v 1−T c)

h fg

,∧x p≥ 0

he πd (Lh+ xp)(T e−T v 1)hfg

,∧x p<0

d mv2

dt={he πd

(Lh−x¿¿ p)(Te−T v 2)hfg

,∧x p ≥0¿hc πd x p(T v2−Tc )

hfg

,∧x p<0

Also C is related to the Reynolds number as:

C=14

¿¿

Solving the above equations given the initial and boundary conditions we can

numerically determine the positon (x p), velocity of the liquid slug and we can

determine the pressures ( pv 1 , pv 2), temperatures (T v 1 , T v 2) and the masses (mv 1 ,m v2)

transiency of the vapor plugs. Algorithm for numerical solution is given below:

1 Given initial values x p0, Lp 0 , d x p

dt 0, T v 10 , T v 20, Pv 10 & Pv 20 find x pand

d x p

dt

using 4th order Runge-kutta method on:

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d2 x p

d t 2 + 2 Cd

(d xp

dt)

2

+ 2gLp

x p=(P¿¿ v1−Pv 2)

Lp ρL

¿

Our functions needed will be equation for Lp(can be assumed constant) and C.

2 We find mass of the vapor plug from the mass balance equation:

d mv1

dt={ −hc πd x p(T v 1−T c)

h fg

,∧x p≥ 0

he πd (Lh+ xp)(T e−T v 1)hfg

,∧x p<0

d mv2

dt={he πd

(Lh−x¿¿ p)(Te−T v 2)hfg

,∧x p ≥0¿hc πd x p(T v2−Tc )

hfg

,∧x p<0

3 We use the energy equation of the vapor plugs to find the temperatures:

mv 1 cv

d T v 1

dt+cv T v 1

d mv 1

dt=−Pv 1 Ac

d x p

dt+

d mv 1

dth fg

mv 2 cv

d T v2

dt+cv T v 2

d mv 2

dt=Pv 2 Ac

d x p

dt+

d mv 2

dth fg

4 We use the temperature , mass and position to find the pressures:

Pv 1(Lh+x p) Ac=mv1 R T v1

Pv 2(Lh−x p) Ac=mv 2 R T v 2

5 In order to find the temperature distribution and transiency of the liquid plug

we use energy equation of liquid slug with the suitable boundary and initial

conditions.

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Chapter 4: Experiment

An experiment was conducted to compare the experimental results and the analytical

solution. The experiment is based on CLPHP. Single loop is considered in our

experiment. Temperature at 8 different locations and pressure at one location has

been found. Snapshot of pulsation at different time is taken. Values for different

filling ratios and different angles are evaluated.

4.1 Experimental Setup

We made a closed pipe of single turn. We needed constant temperature at both ends

(evaporator and condenser), a transparent pipe to see the pulsations happening inside

the pipe. Requirements and what we used are given in the table 4-1.

Table 4-1: Required parts for the experiment

Parts required Parts used

Evaporator to maintain constant

temperature.

Pressure cooker with an electric heater

Condenser to maintain a constant

temperature.

Acrylic box made and ice cold water is

passed through it

Pipes for flow allowing heat transfer in

hater and condenser sides.

Copper tubes

Inlet and outlet for filling and sucking Valves

Transparent adiabatic pipes Glass tubes

Temperature measuring instrument Pre-calibrated thermocouples connected

to a data acquisition system

Pressure measuring instrument Pressure tapping and pressure transducer

Pipes for inlet and outlet to cool the Plastic pipes carrying ice cold water.

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condenser

Filling and sucking mechanism Syringes

4.2 Properties and dimensions of parts used:

Cooker as evaporator:

Figure 4-20: Pressure cooker as evaporator

Copper tubes for conduction of heat:

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Figure 4-21: Copper tube shape and dimensions

Glass tubes for adiabatic past and visualization:

Figure 4-22: Glass tube dimension

Condenser box:

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Figure 4-23: Condenser box made of acrylic plates

Angle setup to give different angle of inclinations:

Figure 4-24: Setup to change the angle of inclination

Thermocouples to measure temperature:

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Eight thermocouples are used to determine the temperatures at 8 different locations of

the CLPHP. Thermocouples were made and calibrated. The accuracy of each

thermocouple is given below:

Table 4-2: Thermocouple accuracy

Thermocouple number Error in °C

1 -1.067

2 -1.295

3 -0.871

4 -1.340

5 -0.904

6 -0.981

7 -0.877

8 -0.914

Pressure tapping to measure pressure:

2 mm tube is used to measure the pressure at one side of the evaporator connecting it

to a pressure transducer.

Fluid:

Alcohol and water is mixed prepared to have a fluid having boiling point temperature

below 95°C. Our 70% to 30% water to alcohol mixture is having a boiling point

temperature as 85°C.

Assembly:

Copper tube is inserted through two holes in the pressure cooker and fixed using m-

seal. One valve is welded to this copper tube outside of the pressure cooker. The

acrylic plates are assembles using chloroform to make the condenser box. Two holes

at the side plates are drilled for cold water inlet and outlet. Plastic pipes are used for

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cold water inlet and outlet. Two more small holes are drilled on the top plate for

inserting thermocouples. Another copper tube is inserted in the condenser box and

fixed with araldite. One valve and one pressure tapping tube (2 mm diameter) is

welded to the copper tube. The glass tubes are connected to the copper tubes using a

nylon seal and araldite. Leaks at each joint were check by blowing air. Araldite or m-

seal is used to prevent leakage. Two thermocouples at both evaporator and condenser

side copper tubes and four thermocouples at four junctions of the glass tube were

fixed using high temperature seal. The assembly was kept on the angle setup plywood

to reduce movements of the parts (which may lead to leakage) and to set different

angle of inclinations. Two water tubs are placed, one above a table and one on the

floor for cold water blowing to cool the condenser. The heater is connected to the

adjustable output voltage distributor through wires.

Figure 4-25: Final assembly

The thermocouples are attached in such a way that the tip of the thermocouples are

just touching the inner flow at the junction of the glass tubes and are touching the

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evaporator and condenser copper tubes externally. Thermocouples are connected to

the data base system and calibrated by dipping the mid-junction in an ice junction so

that we get the values of voltage from the data base system corresponding to 0˚C.

4.3 Procedure

The assembly is kept in the angle setup board at an initial inclined position of about

5-10 degree with the condenser side above. Air is sucked out through the vacuum

valve and closed immediately. Initially water is filled completely to measure the total

volume (glass pipes + copper tubes + other extensions). After measuring, working

fluid (ethanol +water mixture) is filled up to 60% by volume through the filling valve

and closed with the help of two syringes (to fill and suck).

Figure 4-26: (A) Setup to change angle (B) Adjustable voltmeter (0-240 V)

Water is filled in the pressure cooker and the heater is switched on. Output voltage

given to the heater is 220V. Ice cold water (20˚C) from the tub above the table is

passed through the plastic pipes to fill the acrylic box (condenser) and fill the water

tub below. As temperature rises near the boiling point of the working fluid in the

copper tubes (heated section) we try to keep the temperature constant by slowly

decreasing the voltage a little bit. Pulsations are observed in the transparent glass tube

and as the oscillations are somewhat steady we switch on the scan mode in the pre-

configured data acquisition system for extraction of data.

Figure 4-27: (A) Ice bridge (B) Data acquisition system

Temperature variations are extracted as voltage difference and are plotted in the data

acquisition system.

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Figure 4-28: (A) Pressure transducer (B) Connection of glass tubes to condenser

box and cooker

Data (in volts) are exported to excel file and corresponding temperature values are

related by the TC table. These temperature variation with respect to time are plotted

in graphs. Angle of inclination and filling ratio was varied and corresponding

temperature values are extracted to get the results.

4.4 Results

As the pulsations were steady we took the reading at different angles and filling

ratios. The corresponding temperature and pressure values are calculated and

analyzed in the result and discussion section. Snapshots showing the pulsations is in

figure 4-10.

Figure 4-29: Snapshots showing pulsations

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4.5 Probability of errors:

There are some possibility that the results won’t be of high accuracy due to some

fault in our experiment. We have some fault in our setup and some errors due to

environment and instrument errors. Some lengths of conductive copper tube was

exposed to the atmosphere so the adiabatic section was not completely adiabatic. The

filling and sucking valve fittings were longer than usual hence the pressure was not

that precise.

Figure 4-30: Difference between our CLPHP and a typical CLPHP

The temperature of the evaporator and condenser was not exactly constant at 90°C

and 20°C respectively. We tried to keep them constant but some fluctuations occur

due to the environmental effects. The losses due to the sharp bends and tapings of

thermocouples and pressure are also notable. The data extracted for the temperature

from the thermocouples are also having a little error due to the temperature change in

the reference ice bridge due to melting of ice in period of time.

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Chapter 5: Results and Discussion

Our work contains both theoretical and experimental results with some assumptions

and errors respectively. We tried to minimize the experimental errors to get results as

accurate as possible.

5.1 Theoretical results:

Pulsating mode of the various characters e.g. position of vapor bubble, mass of liquid

in the heater section, temperature and pressure of the vapor are seen from the graphs

plotted by the MATLAB program.

Figure 5-31: Position of liquid slug w.r.t time

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Figure 5-32: Velocity of pulsating liquid slug w.r.t time

Initially the pulsation is slow and of small amplitude because the vapors are just

beginning to form as seen in the figure 5-1 and figure 5-2. As time increasers both the

velocity and positional amplitude increases because the pressure difference increases

with time until a steady state is achieved. After the steady state, the amplitude of

position oscillation and velocity is almost constant.

The pressure develops slowly in the heater part with the evaporation of the fluid. For

a fluid of low boiling point evaporation will be fast and hence development of

pressure will be fast. We can see the oscillation of pressure and pressure difference

with time in figure5-3 and 5-4. After steady state the pressure in the vapor oscillates

with almost constant amplitude. The oscillation of pressure in the vapors leads to the

oscillatory motion of the liquid plug.

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Figure 5-33: Pressure of the vapor plugs w.r.t time

Figure 5-34: Pressure difference between the vapor plugs w.r.t time

The temperature of the vapors slowly rises to a value then starts to oscillate. The

phase difference in the oscillation is about 180° which gives a higher temperature in

one vapor and a lower temperature in the other at a particular time and vice versa. By

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the ideal gas law pressure increases with temperature and hence the pressure thrust

moving the liquid slug is pulsating in nature.

Figure 5-35: Temperature of the vapor plugs w.r.t time

We can see that temperature rises slowly at first and after the steady state the

temperature amplitude of both the vapor is constant. Mass of the vapor plug also

changes with the latent heat changes as seen in figure 5-6.

Figure 5-36: Mass of the vapor plugs w.r.t time

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Effect of gravity on the position and velocity of the liquid slug is also found. Effect of

gravity is very less in the behavior of pulsation. For condenser up position increasing

the angle of inclination gives a higher amplitude of both slug position and velocity

and vice versa. As we have taken heater in the top in our model our g=9.8 is the

vertical position with heater at top, g=0 is the horizontal position and g=-9.8 is the

vertical position with condenser at top.

3.50

E-04

1.14

E-02

2.25

E-02

3.35

E-02

4.46

E-02

5.56

E-02

6.67

E-02

7.77

E-02

8.88

E-02

9.98

E-02

1.11

E-01

1.22

E-01

1.33

E-01

1.44

E-01

1.55

E-01

1.66

E-01

1.77

E-01

1.88

E-01

1.99

E-01

2.10

E-01

2.21

E-01

2.32

E-01

2.43

E-01

2.55

E-01

2.66

E-01

2.77

E-01

2.88

E-01

2.99

E-01

3.10

E-01

3.21

E-01

3.32

E-01

3.43

E-01

3.54

E-01

3.65

E-01

3.76

E-01

3.87

E-01

3.98

E-01

-0.3-0.2-0.1

00.10.2

Effect of gravity on slug postion

position g=-9.8 positon g=0 position g=9.8

time in sec

Posi

tion

of l

iqui

d sl

ug

Figure 5-37: Effect of gravity on slug position

3.50E-043.78E-027.52E-021.13E-011.50E-011.87E-012.25E-012.62E-013.00E-013.37E-013.74E-01

-10-8-6-4-202468

10

Effect of gravity on velocity of liquid slug

velocity g=-9.8 velocity g=0 velocity g=9.8

time in sec

Velo

city

of l

iqui

d sl

ug

Figure 5-38: Effect of gravity on slug velocity

The amount of latent and sensible heat transfer is also found.

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5.2 Experimental results

In our experiment we tried to validate our theoretical results and also to find the

effect of filling ratio and gravity in the mode of pulsation. Three filling ratios with

two angles is taken. The results we got explains the reason of an optimum filling ratio

and the effect of gravity at a low temperature gradient.

The position of the thermocouples is shown in the figure

Figure 5-39: Thermocouple location

5.2.1 40% filling ratio:

The fluid we used is a mixture of alcohol and water in the ratio of 1:1. It has a boiling

point around 75-80 degree Celsius. We can see that the pulsation is very slow for

40% filling ratio at a small angle of inclination. The condenser side and evaporator

side thermocouples (1st, 8th, 3rd and 5th) showing almost constant values (figure 5-

10). The 2nd, 4th and 7th thermocouple shows a little oscillation due to the half pulsatile

motion of the liquid slug. The low amount of fluid at this filling ratio leads to less

amount of vapor formation and hence the low pressure in the vapors. This vapor

pressure can’t move the liquid plug hence the gravitational force have to pull the

liquid plug into the heater side. Since the angle is small this process is also very slow.

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0 20 40 60 80 100 1200

0.0005

0.001

0.0015

0.002

0.0025

0.003

0.0035

1001 (VDC) 1002 (VDC) 1003 (VDC) 1004 (VDC) 1005 (VDC) 1006 (VDC)1007 (VDC) 1008 (VDC)

time in seconds

emf i

n m

v

Figure 5-40: Temperature vs time for 40% filling ratio and an angle of

But as we increase the angle of inclination the force due to gravity on the liquid plug

applies pressure on the vapor and comes from the condenser to the heater section and

again vapor is formed and it goes back to the condenser and condenses to liquid and

the cycle continues .this process is slow as it takes time for the pressure development

and condensation of vapor. This is more like a stratified flow rather than slug flow.

0 50 100 150 200 250-0.0005

0

0.0005

0.001

0.0015

0.002

0.0025

0.003

0.0035

1001 (VDC) 1002 (VDC) 1003 (VDC) 1004 (VDC) 1005 (VDC)1006 (VDC) 1007 (VDC) 1008 (VDC)

time in sec

emf n

mv

Figure 5-41: Temperature vs time for 40% filling ratio and an angle of

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5.2.2 80% filling ratio:

Same fluid as before (during 40% filling ratio) is used.

1 6 11 16 21 26 31 36 41 46 51 56 61 66 71 76 81 86 91 96 101 106 111 1160

0.0005

0.001

0.0015

0.002

0.0025

0.003

1001 (VDC) 1002 (VDC) 1003 (VDC) 1004 (VDC)1005 (VDC) 1006 (VDC) 1007 (VDC) 1008 (VDC)

time in sec

emf i

n m

v

Figure shows that the pulsation is very slow, only a small movement is seen in the 8 th

thermocouple. This is because there is not enough vapor inside the pipe to give vapor

pressure for the pulsation to occur and the liquid will stay in the evaporator side for a

long time. Increasing the angle of inclination doesn’t help much as we can see in

figure

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0 20 40 60 80 100 120 1400

0.0005

0.001

0.0015

0.002

0.0025

0.003

0.0035

1001 (VDC) 1002 (VDC) 1003 (VDC) 1004 (VDC)1005 (VDC) 1006 (VDC) 1007 (VDC) 1008 (VDC)

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Chapter 6: Conclusion

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Appendix

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References

1. Thermo-hydrodynamics of closed loop pulsating heat pipes,PHD thesis.

Khandekar, Sameer. 2004.

2. Closed and open loop pulsating heat pipes. Manfred Groll, Sameer Khandekar.

2004.

3. Review and assesment of pulsating heat pipe mechanism for high heat flux

electronic cooling. G. Karimi, J.R. Kulham. s.l. : university of waterloo.

4. Thermal and Visual Observation of Water and Acetone Oscillating Heat Pipes. C.

Wilson, B. Borgmeyer,R. A. Winholtz,H. B. Ma,D. Jacobson,D. Hussey. 2011,

Vol. 133. 061502-5.

5. Theoretical and experimental modelling of an open oscillatory heat pipe including

gravity. Dobson, Robert Thomas. s.l. : University of Stellenbosch, 2003.

6. An open oscillatory heat pipe steam-powered boat. Dobson, Robert Thomson.

s.l. : University of Stellenbosch.

7. Flow and heat transfer of liquid plug and neighboring vapor slugs in a pulsating

heat pipe. Dazhong Yuan, Wei Qu , Tongze Ma. Beijing : Chinese Academy of

Sciences, 2009.

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