planing vessel lecture
TRANSCRIPT
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Planing vessel lecture
O.M.FaltinsenCeSOS,NTNU
Content
• Steady performance• Stepped planing hulls• Dynamic stability• Porpoising• Wave-induced motions• Maneuvering
Planing craftSteamer duckReady for planing !Froude number up to 3Distance up to 1km
Typical planing hull Double-chine hull
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Hard-chine planing hull
Interceptors
2.5D analysis of steady verticalforces = The water entry problem
Drop test of wedge 2D+t representation
Water entry of a wedge Water entry of wedgeTheory and experiments
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Simplified lift (L) calculations
( )3 33df a Vdt
=
( )3 33df U a Udx
τ=
( )233 TL U a xτ=
Consequences of simplified lift formula
• The vessel must have a transom stern and a trim angle to get hydrodynamic lift
• Flow separation from the chines is importantfor trim
( )3 33df U a Udx
τ=
( )233 TL U a xτ=
Design to avoid cavitation,i.edynamic instabilities
• Avoid negative pressuresrelative to atmosphericpressure
• Simplified vertical loadformula gives:
• Avoid convex keel and buttock lines aft of thebow sections
• Careful with how theplaning surface is warped
3 33( )df U a Udx
dzdx
τ
τ
=
= −
Warped planing surface
Savitsky’s formula
0.60 00.0065L L LC C Cβ β= −
1.1 0.5 2.5 20 deg (0.012 0.0055 / )L W W BC Fnτ λ λ= +
2 2
10.755.21 / 2.39
p
W B W
lB Fnλ λ= −
+
Prismatic planing hull
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Planing hulls (Ikeda et al.)Lift force on prismatic planing hull
β = 20ºτ = 4ºλ = 3
1/FnB2
Lift force on prismatic planing hull
β = 20ºτ = 4ºλ = 3
1/FnB2
Hydrostatic force calculations
Lift force and moment on planing vessels
• 2.5D Analysis with flow separation and zero gravity
• 3D Correction in the bow area• Hydrostatic pressure• Suction pressure at the stern
Lift Force on Prismatic Planing Hull
FnB ∞
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Lift Force on Prismatic Planing Hull
FnB ∞
Stepped planing hull
Separation aft ofchine separation
VentilatingRudder
Free-surface-piercing propeller
Flow separation at transom Free-surface profile at the transom
3
2
/ 2 cos(3 / 2)
2S
SU g
Ar
U
X
D
U θ
=
Φ
+
= +
Local analysis offree-surface profile
3/ 2Z AX=
Pressure distribution on the hull
• Infinite pressure gradient at the transomstern
• The local transom stern flow does not match the 2.5D theory
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Savitsky’s empirical formula2 2.44
1 2 3Z X X XC C CB B B B
⎛ ⎞ ⎛ ⎞ ⎛ ⎞= − +⎜ ⎟ ⎜ ⎟ ⎜ ⎟⎝ ⎠ ⎝ ⎠ ⎝ ⎠
20.7deg
1 0.6
2.440.7deg
2 0.6
0.341 deg
0.02064
0.00448
0.0108
B
B
W
CFn
CFn
C
τ
τ
λ τ
⎛ ⎞= ⎜ ⎟⎜ ⎟
⎝ ⎠
⎛ ⎞= ⎜ ⎟⎜ ⎟
⎝ ⎠=
Center-line free-surface profile
2D flat planing surfaceLift force and moment on2D flat planing surface.
2D flat planing surface. Nonlinearities Running attitude and resistance
M=27,000 kglcg=8.84mB=4.27 mDeadrise=10degU=20.58m/s
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Keel and chine wetted lengths
Monohull.Ref.:Per Werenskiold
Heel Angle
Steady roll stability as a function ofspeed
Steady heel instability and chine walking
Φ
0 20
–0.01
0
0.01
0.02
φ(deg)
GZ(m)GZ curve at Fn=0
W=5.31kgmeasured
Fn=1.6
Heel Angle Φ (deg)
Water entry ofheeled section
Simplified water entry analysis ofheeled section
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Porpoising in nature and of planing vessels
Porpoising stability criterion
Porpoising analysis Porpoising
• Equilibrium position for given speed• Stability analysis of coupled linearized
heave and pitch equations withoutexcitation
Porpoising analysis
( )2 2
3 3 5 533 33 33 3 35 35 35 52 2 0d d d dM A B C A B C
dt dt dt dtη η η ηη η+ + + + + + =
tj jae
βη η=
0α >Instability:
iβ α ω= +
( )2 2
3 3 5 553 53 53 3 55 55 55 55 52 2 0d d d dA B C I A B C
dt dt dt dtη η η ηη η+ + + + + + =
Instantaneous position of COG and keel
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Restoring CoefficientsSavitsky´s Formula
Heave force
Restoring CoefficientsSavitsky´s Formula
Pitch moment
Added Mass
• High-frequency strip theory• No forward speed effect
2D infinite frequency heave addedmass
Damping
• No wave radiation• Hull lift damping. Use lift part of Savitsky’s
formula in a quasi-steady analysis
Example heave
Effect of lcg on porpoising
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Porpoising.Sensitivity to hydrodynamic coefficients
Stability parameter <0 Porpoising
Planing boat in waves
Vertical accelerations of 57-foot boat in sea state 5 Generalized Froude Kriloff loads
sin( )a et kxζ ζ ω= −
sin cos cos sin sin cosa e a e a e a et kx t kx t xk tζ ζ ω ζ ω ζ ω ζ ω= − ≈ −
3 33 35sin cosFKa e a eF C t C k tζ ω ζ ω= +
5 53 55sin cosFKa e a eF C t C k tζ ω ζ ω= +
Long wave length approximation ofwave excitation
Resonant wave length condition
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Strong nonlinearities in shipmotions of a planing craft
Heave/Wave amplitude
Wave length/L
Maneuvering
Steady turning motion GZ during turning