Hydrodynamics
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[2009] [09] [10]
Innovative ship design
- Ship Motion & Wave Load -
April, 2009
Prof. Kyu-Yeul Lee
Department of Naval Architecture and Ocean Engineering, Seoul National University of College of Engineering
서울대학교 조선해양공학과 학부4학년 “창의적 선박설계” 강의 교재
Hydrodynamics
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N av al A rc hite ctu re & O ce an E ngin ee rin g
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National Univ.
Chap.1 Loads acting on a ship
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Ship Structural Design
Ship Structural Design
what is designer’s major interest?
Safety :
Won’t ‘IT’ fail under the load?
L
x
y f x ( )
( ) f x
x
y
react
F
( ) V x
( ) M x
( ) y x
Differential equations of the defection curve 4
4
( ) ( ) d y x
EI f x
dx = − what is our interest?
: ( ) : ( ) : ( ) Shear Force V x Bending Moment M x Deflection y x
: ( ) Load f x
cause
( ) ( ) dV x f x
dx = − ( )
, dM x ( ) dx = V x
2
2
, d y x ( ) ( )
EI M x
dx =
‘relations’ of load, S.F., B.M., and deflection
Safety :
Won’t it fail under the load?
Geometry :
How much it would be bent under the load?
,
acty i
M M
where
I y Z
σ = =
act l
σ
≤σ
Stress should meet :
a ship a stiffener a plate
global local
σ
act: Actual Stress
σ
t: Allowable Stress
Hydrodynamics
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4 /203
Ship Structural Design
Ship Structural Design
what is designer’s major interest?
Safety :
Won’t ‘IT’ fail under the load?
a ship a stiffener a plate
L
x
y f x ( )
global local
a ship
Actual stress on midship section should be less than allowable stress
l
act σ
σ . ≤
Allowable stress by Rule (for example):
2
, σ
l= 175 f
1[ N mm / ]
, act . S W mid
M M
σ Z
= + Hydrostatics
L
x
y f x ( )
( ) f x
x
y
react
F
( ) V x
( ) M x
( ) y x
Differential equations of the defection curve 4
4
( ) ( ) d y x
EI f x
dx = − what is our interest?
: ( ) : ( ) : ( ) Shear Force V x Bending Moment M x Deflection y x
: ( ) Load f x
cause
( ) ( ) dV x f x
dx = − ( )
, dM x ( ) dx = V x
2
2
, d y x ( ) ( )
EI M x
dx =
‘relations’ of load, S.F., B.M., and deflection
Safety :
Won’t it fail under the load?
Geometry :
How much it would be bent under the load?
,
acty i
M M
where
I y Z
σ = =
Stress should meet :
σ
act: Actual Stress σ
t: Allowable Stress
act l
σ
≤σ
M
S= Still water bending moment
M
W= Vertical wave bending moment Hydrodynamics
z
x
what kinds of load
cause hull girder moment?
f
Hydrodynamics
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Ship Structural Design
Ship Structural Design
what is designer’s major interest?
Safety :
Won’t ‘IT’ fail under the load?
a ship a stiffener a plate
global local
a ship
L
x
y f x ( )
( ) f x
x
y
react
F
( ) V x
( ) M x
( ) y x
Differential equations of the defection curve 4
4
( ) ( ) d y x
EI f x
dx = − what is our interest?
: ( ) : ( ) : ( ) Shear Force V x Bending Moment M x Deflection y x
: ( ) Load f x
cause
( ) ( ) dV x f x
dx = − ( )
, dM x ( ) dx = V x
2
2
, d y x ( ) ( )
EI M x
dx =
‘relations’ of load, S.F., B.M., and deflection
Safety :
Won’t it fail under the load?
Geometry :
How much it would be bent under the load?
,
acty i
M M
where
I y Z
σ = =
Stress should meet :
σ
act: Actual Stress σ
t: Allowable Stress
act l
σ
≤σ
S ( ) f x
,
act . S W mid
M M
σ Z
= +
l
act σ
σ . ≤
: load in still water
( )
0x( )
S S
V x = ∫ f x dx
S ( ) V x
S ( ) M x
( )
0x( )
S S
M x = ∫ V x dx
Hydrostatics Hydrodynamics
. F K diffraction added mass
mass inertia
damping: still water shear force
: still water bending moment
, M
S= Still water bending moment M
W= Vertical wave bending moment what kinds of load f cause hull girder moment?
weight
buoyancy
f S (x) : load in still water
= weight + buoyancy
W ( )
f x : load in wave
( )
0x( )
W W
V x = ∫ f x dx
W ( ) V x
W ( )
M x
( )
0x( )
W W
M x = ∫ V x dx
: wave shear force
: vertical wave bending moment
f
W(x) : load in wave
= added mass + diffraction
+ damping + Froude-Krylov + mass inertia ( )
S( )
W( ) f x = f x + f x
( )
S( )
W( ) V x = V x + V x
( )
S( )
W( )
M x = M x + M x
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1. Loads acting on a ship (1) - Loads in still water
z
x
x ( ) z
w x w(x):weight
x ( ) z
b x
+
b(x):bouyancy
In still water
( ) ( ) ( ) f S x = b x − w x
what kinds of load f S cause ? M s
( ) S ( ) W ( ) f x = f x + f x
x
( ) z f S x
f
S(x)= b(x) – w(x) : Load
=
b(x) : buoyancy distribution in longitudinal direction w(x) = LWT(x) + DWT(x)
- w(x) : weight distribution in longitudinal direction - LWT(x) : lightweight distribution
- DWT(x) : deadweight distribution
(M
S:Still water bending Moment in midship)
f(x) : distribution load in longitudinal direction
f S (x) : distribution load in longitudinal direction in still water
f W (x) : distribution load in longitudinal direction in wave
Hydrodynamics
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1. Loads acting on a ship (2)
- Example of 3,700TEU Container carrier
Load Curve, f
S(x) Still water
Shear Force, V
S(x)
Still water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
- Frame space : 800mm
Example of 3,700 TEU Container Ship in Homogeneous 10t Scantling Condition - Principal dimensions & drawings
- Loading Condition (Sailing state) in homogeneous 10t scantling condition
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
- principal dimension - profile & plan drawing - midship section
Hydrodynamics
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LIGHTWEIGHT DISTRIBUTION DIAGRAM
FR. NO 0 25 50 74 99 125 150 175 200 226 251 276 301 326 0.0
20.0 40.0 60.0 80.0 100.0 120.0 140.0 160.0 180.0 200.0 220.0 240.0 TONNES
Crane
Bow Thruster Emergency
Pump Engine
(Example of 3,700TEU Container carrier)
1. Loads acting on a ship (2) - Lightweight
AP FP
E/R
A.P F.P
Load Curve, f
S(x) Still water
Shear Force, V
S(x)
Still water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
Hydrodynamics
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- Loading Plan in homogenous 10t scantling condition
1. Loads acting on a ship (3) - Deadweight
(Example of 3,700TEU Container carrier)
Deadweight distribution in longitudinal direction in homogenous 10t scantling condition
- Deadweight distribution curve in homogenous 10t scantling condition
A.P FR.Space : 800 mm F.P
Load Curve, f
S(x) Still water
Shear Force, V
S(x)
Still water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
Hydrodynamics
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(2) 면적 길이 방향으로 적분하여 부피 계산
(1) 수선면 아래의 선박 단면적계산
x
A
' y
' z
Buoyancy Curve in Homogeneous 10ton Scantling Condition
1. Loads acting on a ship (4) - Buoyancy curve
(Example of 3,700TEU Container carrier)
100 ton
FR.No
A.P F.P
FR.Space : 800 mm
Buoyancy 계산방법
Load Curve, f
S(x) Still water
Shear Force, V
S(x)
Still water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
Hydrodynamics
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11 /203 LIGHTWEIGHT DISTRIBUTION DIAGRAM
FR. NO 0 25 50 74 99 125150175 200226 251276301 326 0.0
20.0 40.0 60.0 80.0 100.0 120.0 140.0 160.0 180.0 200.0 220.0 240.0 TONNES
=Lightweight + Deadweight
Load Curve
Still Water shear Force
Load Curve
=Weight+ Buoyancy
+
+
=
Bouyancy Curve Weight curve
S ( ) f x
1. Loads acting on a ship (5) - Load/Shear/Moment curve
(Example of 3,700TEU Container carrier)
Lightweight Distribution Curve Deadweight Distribution Curve
FR.No
A.P F.P A.P F.P
A.P FR.Space : 800 mm F.P
100 ton
FR.No
A.P F.P
FR.Space : 800 mm A.P F.P
= Weight w(x) + Buoyancy b(x)
Load Curve, f
S(x) Still Water Shear Force, V
S(x)
Still Water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
in homogenous 10t scantling condition
in homogenous 10t scantling conditi on in homogenous 10t scantling condition
in homogenous 10t scantling condition
Hydrodynamics
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Shear force
Permissible shear force
Still Water Shear Curve
Bending Moment Permissible Bending Moment
Still Water Bending
Moment Curve Load Curve
Actual still water shear force is lower than permissible Shear.
→ O.K
Actual still water bending moment is lower than permissible bending.
→ O.K
( ) ( ) ( ) f S x = b x − w x
( ) 0 x ( )
S S
V x = ∫ f x dx
1. Loads acting on a ship (6) - Load/Shear/Moment curve
(Example of 3,700TEU Container carrier)
( )
0 x
( )S S
M x
=∫ V x dx
Load Curve, f
S(x) Still water
Shear Force, V
S(x)
Still water
Bending Moment, M
S(x) Weight, w(x)
Buoyancy, b(x)
( )
0x( )
S S
V x = ∫ f x dx M
S( ) x = ∫
0xV x dx
S( )
Hydrodynamics
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33 3 33 3
( ) ( ) ( )
f R x = − a x ξ − b x ξ
How to know ?
ξ ξ 3 , 3 z
x
z
x
In still water
In wave
( ) ( ) ( ) f S x = b x − w x
( ) ( )
( ) S W
f x = f x + f x
3 .
( ) ( ) ( ) (
( ) ( ) m x f D x f F K x f R x )
b x w x − ξ + + +
= −
x
( ) z
f
Wx
?
2. Loads in wave
• for example, consider heave motion
• from 6DOF motion of ship
[ ξ 1 , ξ 2 , ξ 3 , ξ 4 , ξ 5 , ξ 6 ] T
= x
ξ 3
x
( ) z f
Sx
f
S(x)= b(x) – w(x) : Load
+
f
D(x) : Diffraction force in a unit length f
R(x) : Radiation force in a unit length f
F.K(x) : Froude-Krylov force in a unit length
Where,
Roll ξ
4Pitch ξ
5Hea ve ξ
3Yaw ξ
6O
x y
z
ref.> 6 DOF motion of ship
additional loads in wave
Loads in wave
In order to know loads in wave, we have to know ξ ξ
3,
3f(x) : Distribution load in longitudinal direction
f
S(x) : Distribution load in longitudinal direction in still water
f
W(x) : Distribution load in longitudinal direction in wave
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3. 6DOF Equation of motion of ship
R D I
Φ Φ
Φ : Incident wave velocity potential : Diffraction wave velocity potential : Radiation wave velocity potential F
F.K: Froude-krylov force
F
D: Diffraction force F
R: Radiation force
matrix coeff.
restoring 6
6 :
matrix coeff.
damping 6
6 :
matrix mass
added 6 6 :
×
×
×
C B M
A 선박에 작용 하는 유체력
.
Static + F K + D + R
F F F F
Gravity +
= F x M
Restoring
F F Wave exciting F R = − Ax Bx −
, ,
( Gravity Static ) Wave exciting External dynamic External static
= + + − − + +
Mx F F F Ax Bx F F
( M + A x Bx Cx ) + + = F Wave exciting + F External dynamic , + F External static ,
Linearization
, (F Restoring
= (F Gravity
+F Static
)≈ −Cx
)added
mass Damping Coefficient Surface force
Body force
, ,
External dynamic External static
+ F + F
Wave exciting force를 제외한 외력(ex. 제어력 등)
( )
B B B
I D R
Fluid
S P dS ρgz dS S S dS
t t t
ρ
∂Φ ∂Φ ∂Φ= = − − + +
∂ ∂ ∂
∫∫ ∫∫ ∫∫
F n n
선박의 6자유도 운동방정식
Newton’s 2nd
Law=
= ∑ F
x M
Gravity Fluid
= F + F
F Body
+ FSurface
External
+F
선박의 Surface force로 작용
How to know ?
3 , 3
ξ ξ
Fluid
Pρgz = − − ρ ∂Φ t
∂
∂ Φ + ∂
∂ Φ + ∂
∂ Φ
− ∂
−
= ρgz ρ t
It
Dt
RBy solving equation of motion, we could know the velocities, accelerations!!
선박에 작용하는 압력
Static
=
F
+F F K .
+F D
+F R
Linearized Bernoulli Eq.
By solving equation of motion,
we could know the velocities,
accelerations.
Hydrodynamics
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N av al A rc hite ctu re & O ce an E ngin ee rin g
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Chap 2.
6 DOF Equations of Ship Motion
Hydrodynamics
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Coordinate system [ ]
T 6 1 , , ξ ξ
=
(변위 : ) x
O-xyz : Global coordinate system
① right-handed coordinate system (O-x,y,z)
origin in the plane of the undisturbed free-surface
② if body moves with a mean forward speed, coordinate moves with the same speed
③ body have the x-z plane as a plane of symmetry
O’-x’ y’ z’ : Body-fixed coordinate system
G : Position of center of gravity y
z
G O
y′ c
z′ c
x
c,y
c,z
c: distance from O’-x’y’z’ to center of gravity
U Roll ξ
4Pitch ξ
5Hea ve ξ
3Yaw ξ
6O G
x y
z z′
2
y′
ξ
ξ
3ξ
4O′
x z
O
x′
z′
O′ G
x′ c
z′ c
ξ 1
ξ 3
ξ
5
1) Newman, J.N. , Marine Hydrodynamics, The MIT Press, Cambridge, 1977, pp 285~290
Hydrodynamics
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Uncoupled Heave motion equation
Heave 운동 방정식 유도
B W
restore damping F
F
z
Z
X
평형상태에서
더 들어간 부피
= F gravity + F static + F F . K + F D + F R
Fluid gravity
Surface Body
F F
F F
F M
+
=
+
=
= ∑
ξ 3
exciting,3
F
3 33 3
33 ξ B ξ
A −
3 −
0 ρ ξ
ρ gV − gA wp ⋅
− Mg
3 33 3
33 3
, 3
0 )
( ρ gV ρ gA ξ F A ξ B ξ
Mg + − wp + exciting − −
−
=
3 , 3
3 33 3
33 )
( M + A + B + gA wp = F exciting
∴ ξ ξ ρ ξ
Surge 운동 방정식 유도
(Heave에서 복원력 성분만 제외)
1 , 1
11 1
11 )
( M + A + B = F exciting
∴ ξ ξ
Sway 운동 방정식 유도
(Heave에서 복원력 성분만 제외)
2 , 2
22 2
22 )
( M + A + B = F exciting
∴ ξ ξ
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Uncoupled Heave motion equation 풀이
ex) For Heave motion
( M + A 33 ) ξ 3 + B 33 ξ 3 + C 33 ξ 3 = F exciting , 3
t i A t
i A t
i A t
i
A e B i e C e f e
A
M 33 )( ω 2 ξ 3 ω ) 33 ( ω ξ 3 ω ) 33 ( ξ 3 ω ) η 0 3 ω
( + − + + =
t i A e t ξ ω ξ 3 ( ) = 3
t i A e i
t ω ξ ω ξ 3 ( ) = 3
t i A e t ω ξ ω ξ 3 ( ) = − 2 3
t i A t
i A
exciting F e f e
F , 3 = 3 ω = η 0 3 ω
( : Wave Amplitude, Real), (ξ η 0 3 A : Amplitude of heave motion, Complex) ( : 1m 파고에 대한 Wave exciting force Amplitude, Complex) f 3 A
Assumption :
시간이 충분히 흘러steady 상태에서, 선박이 외력의 주파수
ω 와 같은 운동을 함(Harmonic Motion) -> 초기 Transient Motion은 고려하지 않음.
{ ω M A 33 i ω B 33 C 33 } ξ 3 A e i ω t η 0 f 3 A e i ω t
2 ( + ) + + =
−
= D
{ M A 33 i B 33 C 33 } 3 A 0 f 3 A
2 ( ) ω ξ η
ω + + + =
− 1
3 0 3
= f A D −
A η
ξ 3 1
0
3 = A D − A
η f ξ
RAO (Response Amplitude Operator)
: 1m wave Amplitude 를 가지는 주파수 ω인 wave에 대한
heave운동 변위의 진폭
( Complex)
1) Newman, J.N. , Marine Hydrodynamics, The MIT Press, Cambridge, 1977, pp 307~310
동일한 항으로 정리가능
( : Wave exciting frequency) ω
,( A
33: heave motion에 의한 heave 방향 added mass)
,( B
33: heave motion에 의한 heave 방향 damping coefficient)
,( C
33: heave motion에 의한 heave 방향 복원력 coefficient)
,( M :Mass of ship)
Hydrodynamics
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Uncoupled roll motion equation
Roll 운동 방정식 유도
Fluid gravity
Surface Body
xx
M M
M M
M I
+
=
+
=
= ∑
ξ 4
R D
K F static
gravity M M M M
M + + + +
= .
exciting,4
M
4 44 4
44 ξ B ξ
A −
− k
r × ∆
B
1k r G × W
4 44 4
44 4
, A ξ B ξ M
GZ + exciting − −
⋅
∆
=
,
GZ
= −y G
+y B
1O
y z
τ
(+ )
B G
z
′y
′K
C L
y z
F ∆
B 1
B
1r
g 1 g
W
M T
τ
er G
Z
W r
Gγ
GO
restoring
τ
ξ 4
ξ 4
F
∆B1
r
B1
γ
γ π − O
γ γ π ) sin sin( − =
+ π
γ 2 π
γ − π − x sin
x
M
T: B Global
1을 지나는 부력 작용선과 선체 중심선과의 교점 coordinate oyz
coordinate fixed
Body z
oy :
:
'
'
Hydrodynamics
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Uncoupled Roll motion equation
Roll 운동 방정식 유도
Fluid gravity
Surface Body
xx
M M
M M
M I
+
=
+
=
= ∑
ξ 4
R D
K F static
gravity M M M M
M + + + +
= .
exciting,4
M
4 44 4
44 ξ B ξ
A −
− k
r × ∆
B
1k r G × W
4 44 4
44 4
, A ξ B ξ M
GZ + exciting − −
⋅
∆
=
4 44 4
44 4
,
sin ξ 4 M A ξ B ξ
GM + exciting − −
⋅
∆
−
=
4 44 4
44 4
,
4 ξ ξ
ξ M A B
GM + exciting − −
⋅
∆
−
≈
44 44 4 44 4 4 ,4
( I A ) ξ B ξ GM T ξ M exciting
∴ + + + ∆ ⋅ =
Pitch 운동 방정식 유도 (Roll 운동 방정식과 동일)
Yaw 운동 방정식 유도
(RollHeave에서 복원력 성분만 제외)
sin 4
GZ
GM ξ
= −
4
sin ξ 4 ≈ ξ
55 55 5 55 5 5 ,5
( I A ) ξ B ξ GM L ξ M exciting
∴ + + + ∆ ⋅ =
66 66 6 66 6 ,6
( I A ) ξ B ξ M exciting
∴ + + =
O
B G
z ′
y ′
K
C L
y z
F ∆
B 1
g 1 g
W M T
Z
W
F
∆B1
r
B1
γ
γ O π −
γ γ π
) sin sin( − =+ π
γ 2π
γ − π− x sin
x
M
T: B Global
1을 지나는 부력 작용선과 선체 중심선과의 교점 coordinate oyz
coordinate fixed
Body z oy
:
:
'
'
Hydrodynamics
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National Univ.
21 /203
Uncoupled Pitch motion equation
For Pitch motion
( A 55 + I 55 ) ξ 5 + B 55 5 ξ + C 55 5 ξ = F exciting ,5
2
55 55 5 55 5 55 5 0 5
( A + I )( − ω ξ A i t e ω ) + B ⋅ ( i ωξ A i t e ω ) + C ⋅ ( ξ A e i t ω ) = η f e A i t ω
5 ( ) t 5 A i t e ω ξ = ξ
5 ( ) t i 5 A i t e ω ξ = ωξ
2
5 ( ) t 5 A i t e ω ξ = − ω ξ
,5 5 0 5
A i t A i t
exciting
F = F e ω = η f e ω
( : Wave Amplitude, Real), (ξ η 0 5 A : Amplitude of pitch motion, Complex) ( : 1m 파고에 대한 Wave exciting force Amplitude, Complex) f 5 A
Assumption :
시간이 충분히 흘러steady 상태에서, 선박이 외력의 주파수
ω 와 같은 운동을 함(Harmonic Motion) -> 초기 Transient Motion은 고려하지 않음.
{ − ω 2 ( A 55 + I 55 ) + i B ω 55 + C 55 } ξ 5 A i t e ω = η 0 f e 5 A i t ω
= D
{ − ω 2 ( A 55 + I 55 ) + i B ω 55 + C 55 } ξ 5 A = η 0 f 5 A ξ 5 A = η 0 f D 5 A − 1 5 5 1
0 A
f A
ξ η
= D −
RAO (Response Amplitude Operator)
: 1m wave Amplitude 를 가지는 주파수 ω인 wave에 대한
pitch운동 변위의 진폭
( Complex)
1) Newman, J.N. , Marine Hydrodynamics, The MIT Press, Cambridge, 1977, pp 307~310
동일한 항으로 정리가능
( : Wave exciting frequency) ω
,( A
55: pitch motion에 의한 pitch 방향 added mass)
,( B
55: pitch motion에 의한 pitch 방향 damping coefficient)
,( C
55: pitch motion에 의한 pitch 방향 복원력 coefficient)
,( I
55: Mass moment of inertia of ship with respect to y axis)
Hydrodynamics
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National Univ.
22 /203
Motion of any point on the body - Acceleration of any point
Position vector of any point about the Origin(O)
T
′R
′= + + ×
x ξxξx
Translatory displacements of body fixed coordinate in the x-,y-, and z-directions with respect to the origin(O)
Angular displacements of rotational motion in the x-,y-, z- axis with respect to the origin(O)
4 5 6
R = ξ + ξ + ξ
ξi j k
,(Surge, Sway, Heave)
,(Roll, Pitch, Yaw)
4 5 6
,
Rx y z
ξ ξ ξ
× = ′
′ ′ ′
i j k
ξx
x-,y-,z- acceleration are coupled with other motions
G′
G
ξ
5 x′
z′
' O O
z
x′
Heave motion caused by pitch motion Similarly, roll motion cause heave motion
( ξ
1z ′ ξ
5y ′ ξ
6) ( ξ
2z ′ ξ
4x ′ ξ
6) ( ξ
3y ′ ξ
4x ′ ξ
5)
= + − + − + + + −
x i j k
ex.) Acceleration of heave motion :
x′ G
G′
ξ
5O
5 1
x
cξ ≈ k z
1
s z
If ξ
5is small,
s ≈ k z
1k i
( ξ
3+ y ′ ξ
4− x ′ ξ
5) k ( ξ
3+ y ′ ξ
4− x ′ ξ
5) k
① : heave acceleration ② heave acceleration by roll
③ : heave acceleration by pitch
① + ② + ③
Find : Acceleration of any point x
Motion of equation :
1 2 3
T = ξ + ξ + ξ
ξi j k
( : position vector with respect to O’-x’y’z’ coordinate) ( : position vector with respect to O-xyz coordinate)
x y z
′ = ′ + ′ + ′
x i j k
x y z
= + +
x i j k
restoring exciting radiation
M x = F + F + F
T
′R
′R
′= + + × + ×
x
ξxξxξx
Velocity vector
Acceleration vector
( )
2
T R R R R
T R R R
′ ′ ′ ′ ′
= + + × + × + × + ×
′ ′ ′ ′
= + + × + × + ×
x ξxξxξxξxξx ξxξxξxξx
선박을 강체로 가정하면, 선박 위의 한 점은 시간에 따라 변하지 않는다
T R
′= + ×
x ξξx
( ξ
1z ′ ξ
5y ′ ξ
6) ( ξ
2z ′ ξ
4x ′ ξ
6) ( ξ
3y ′ ξ
4x ′ ξ
5)
= + − i + − + j + + − k
1) Newman, J.N. , Marine Hydrodynamics, The MIT Press, Cambridge, 1977, pp 307~310
Hydrodynamics
@ SDAL
Advanced Ship Design Automation Lab.http://asdal.snu.ac.kr Seoul
National Univ.
23 /203
Motion of any point on the body
- (참조) Acceleration of any point Find : Acceleration of any point x
Motion of equation :
restoring exciting radiation
M x = F + F + F
Position vector of any point about the Origin(O)
T
′
R′
= + + ×
xξxξx
( Translatory displacements : ξ
T= ξ
1i+ ξ
2j+ ξ
3k , (Surge, Sway, Heave) ) ( Angular displacements : ξ
R=ξ
4i+ ξ
5j+ ξ
6k , (Roll, Pitch, Yaw) )
4 5 6
,
Rx y z
ξ ξ ξ
× = ′
′ ′ ′
i j k
ξx
O
T O′
′
= +
xξR x
Position vector of any point about the Origin(O)
6 6
1
6 6
2
cos sin sin cos
x x
y y
ξ ξ
ξ
ξ ξ
ξ
′
−
= +
′
6 6
1
6 6
2
cos sin
sin cos
x y
x
x y
y
ξ ξ
ξ
ξ ξ
ξ
′ −
= +
′ + ′
If we consider 2-dimensional motion
If we consider 2-dimensional motion
1
6 2
0 0 0
x x
y y
x y
ξ ξ
ξ
′
= + +
′
′ ′
i j k
6 1
6 2
y
x x
x
y y
ξ ξ
ξ ξ
′ − ′
= + +
′ + ′
6 1
6 2
x y x
y x y
ξ ξ
ξ ξ
′ − ′
= +
′ + ′
Linearize (cosθ→1, sinθ→θ)
x′
O′
y′
P′
Inertial frame (O-frame)
y
O x
[ x y , ]
T′ = ′ ′ x
i O
j O
k O
i O′
j O′
k O′
ξ
6[ ]
x y ,
T= x
[ 1 , 2 ] T
T = ξ ξ
ξ
(병진운동)(회전운동)
x′
O′
y′
P′
Inertial frame (O-frame)
y
O x
[ x y , ]
T′ = ′ ′ x
i O
j O
k O
i O′
j O′
k O′
ξ
6[ ]
x y ,
T= x
[ 1 , 2 ] T
T = ξ ξ
ξ
(병진운동)(회전운동)
× ′ ξx
P
If summing the body motions ξ j are small and neglecting,
Linearize
ξ
Rx ′
R
× ′
ξx
Hydrodynamics
@ SDAL
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National Univ.
24 /203
Motion of any point on the body
- (참조) Acceleration of any point Find : Acceleration of any point x
Motion of equation :
restoring exciting radiation
M x = F + F + F
Position vector of any point about the Origin(O)
T
′
R′
= + + ×
xξxξx
T
′
R′
R′
= + + × + ×
xξxξxξx
Velocity vector
Acceleration vector
T
′
R′
R′
R′
R′
= + + × + × + × + ×
x ξxξxξxξxξx
O
T O′
′
= +
x ξR x
O O
T O O
O O
T O O
d dt
ω
′ ′
′ ′
′ ′
= + +
′ ′
= + × +
x ξR x R x ξR x R x
( ) ( )
2
2
O O O O O
T O O O O O
d
dt x = + ω ×
′′ + × ω
′′ + × ω
′′ +
′′ +
′′ ξR x R x R x R x R x
Position vector of any point about the Origin(O)
Velocity vector
Acceleration vector
①E-frame 에 대한
점 P의 가속도
( Translatory displacements : ξ
T= ξ
1i+ ξ
2j+ ξ
3k , (Surge, Sway, Heave) ) ( Angular displacements : ξ
R=ξ
4i+ ξ
5j+ ξ
6k , (Roll, Pitch, Yaw) )
22 T O O O O
2
O O O Od
dt x = + × ω
′′ + × × ω ω
′′ + ω ×
′′ +
′′
ξR x R x R x R x x ξxξxξxξx = T + + ′ R × + ′ 2 ( R × ′ ) + R × ′
x′
O′
y′
P′
Inertial frame (O-frame)
y
O x
[ x y , ]
T′ = ′ ′ x
i
Oj
Ok
Oi
O′j
O′k
O′ξ
6[ ]
x y, Tx=
[
1,
2]
TT
= ξ ξ
ξ
(병진운동)(회전운동)
x′
O′
y′
P′
Inertial frame (O-frame)
y
O x
[ x y , ]
T′ = ′ ′ x
i
Oj
Ok
Oi
O′j
O′k
O′ξ
6[ ]
x y, T= x
[
1,
2]
TT
= ξ ξ
ξ
(병진운동)(회전운동)
× ′ ξx
P
Linearize
② E-frame 에 대한
A-frame의 원점
A의 가속도 ⑥ A-frame 를 고정시켜 놓았을 때,
A-frame 에 대한
점 P의 가속도
③A-frame이 각 가속도를 가지고 회전하고 있을 때, 점 P의 접선 방향의 가속도
④A-frame이 회전하고 있 을 때, 점 P의 회전 중심 방향의 가속도 (구심력)
⑤ Coriolis Acceleration (Coriolis Effect) 회전 좌표계에서 기술된움직이는
점을 고정 좌표계에서 바라봤을 때,발생하는 효과
O O O O O
T
ω
O′′ ω ω
O′′ ω
O′′ ω
O′′
O′′
= ξR x + × + × × R x R x + × R x + × R x + ⑥ A-frame 를 고정시켜 놓았을 때,
A-frame 에 대한점 P의 가속도
⑤ Coriolis Acceleration (Coriolis Effect) 회전 좌표계에서 기술된움직이는
점을 고정 좌표계에서 바라봤을 때,발생하는 효과
③A-frame이 각 가속도를 가지고 회전하고 있을 때, 점 P의 접선 방향의 가속도
② E-frame 에 대한
A-frame의 원점 A의 가속도
①E-frame에 대한
점 P의 가속도
(선형화한 가정으로 인해 구심가속도 성분이 나타나지 않음)
Hydrodynamics
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National Univ.
25 /203
( 2 64 4 66 6 )
yaw = M x c I I
τ ′ + ξ ξ + ξ k
( 1 1 2 3 55 5 )
= +
=
pitch pitch pitch
c c
M z M x I
τ τ τ
ξ ξ ξ
′ − ′ + j
( 2 44 4 46 6 )
roll = M z c I I
τ − ′ ξ + ξ + ξ i
2 = 1 3
pitch z c M x c M
τ k × ξ i + i × ξ k
Moment in pitch motion
1) Journee, J.M.J. , Adegeest, L.J.M. ,Theoretical Manual of Strip Theory program“ Seaway for Windows”, Delft University of Technology, 2003, pp38~42 2) 구종도 역, 선체와 해양구조물의 운동학, 연경문화사, pp68~71
Moment in pitch motion
(with respect to y-axis)
Find : Moment
restoring exciting radiation
I
ω = M + M + M I
ω
Motion of equation for roll, pitch, yaw
x′
z′
O′
G
x′ c
z′ c
M
ξ 3
M
ξ 1
5
I yy
ξ
1
55 5 pitch = I
I τ
ξ
= ω
j
Moment by mass moment of inertia
( 1 3 )
= M z moment arm c ξ − M x c ξ j
force
Moment by inertia force
, ( I : mass moment of inertia ) , ( : Angular acceleration ) ω
Moment in pitch motion
Moment in roll motion
(with respect to x-axis, y
c=0 according to Lateral Symmetric)
Moment in yaw motion(with respect to z-axis , y
c=0 according to Lateral Symmetric)
[ ξ 1 , ξ 2 , ξ 3 , ξ 4 , ξ 5 , ξ 6 ] T
= x
heave sway surge
: : :
3 2 1
ξ ξ ξ
yaw pitch roll
: : :
5 4 3
ξ ξ ξ
x'
c,y’
c,z’
c: distance from O’-x’y’z’ to center of gravity
O
z
Hydrodynamics
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National Univ.
26 /203
Mass moment of inertia
1) Journee, J.M.J. , Adegeest, L.J.M. ,Theoretical Manual of Strip Theory program“ Seaway for Windows”, Delft University of Technology, 2003, pp38~42 2) 구종도 역, 선체와 해양구조물의 운동학, 연경문화사, pp68~71
mass moment of Inertia
2 2
44 ( )
V
I = ∫∫∫
ρy + z dV , 55 ( 2 2 )
V
I = ∫∫∫
ρx + z dV , 55 ( 2 2 )
V
I = ∫∫∫
ρx + y dV
46 V
I = ∫∫∫
ρxzdV , 45 ...
V
I = ∫∫∫
ρxydV
관성 모멘트는 계산하기 위해 많은 정보가 필요하여 , 계산이 복잡하다.
따라서 자료가 주어지거나 추정식을 사용하여 구한다 . (m=ρ▽)
2 2 2
44 44 , 55 55 , 66 66 ,
I = k
ρ∇ I = k
ρ∇ I = k
ρ∇
- 추정식① 1)
44 55 66
0.30 to 0.40 0.22 to 0.28 0.22 to 0.28
k B B
k L L
k L L
≈
≈
≈
- 추정식② 1) (Proposal of Bureau Veritas)
244