Chapter IV (Ship Hydro-Statics & Dynamics) Floatation & - - PDF document

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Chapter IV (Ship Hydro-Statics & Dynamics) Floatation & Stability

4.1 Important Hydro-Static Curves or Relations (see Fig. 4.11 at p44 & handout)

• Displacement Curves (displacement [molded, total]
• vs. draft, weight [SW, FW] vs. draft (T))
• Coefficients Curves (CB , CM , CP , CWL, vs. T)
• VCB (KB, ZB): Vertical distance of Center of

Buoyancy (C.B) to the baseline vs. T

• LCB (LCF, XB): Longitudinal Distance of C.B or

floatation center (C.F) to the midship vs. T

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4.1 Important Hydro-Static Curves or Relations (Continue)

• TPI: Tons per inch vs. T (increase in buoyancy due

to per inch increase in draft)

• Bonbjean Curves (p63-66)

a) Outline profile of a hull b) Curves of areas of transverse sections (stations) c) Drafts scales d) Purpose: compute disp. & C.B., when the vessel has 1) a large trim, or 2)is poised on a big wave crest or trough.

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How to use Bonjean Curves

• Draw the given W.L.
• Find the intersection of the W.L. & each station
• Find the immersed area of each station
• Use numerical integration to find the disp. and C.B.

4.2 How to Compute these curves

• Formulas for Area, Moments & Moments of Inertia

2 2 2 2 .

) Area , ) Moments , Center of Floatation / ) Moments of Inertia ,

L A L M I A L C F

a d ydx A ydx b d xydx M xydx x M A c d x d x ydx I x ydx I I x A          

  

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Examples of Hand Computation of Displacement Sheet (Foundation for Numerical Programming)

• Area, floatation, etc of 24’ WL (Waterplane)
• Displacement (molded) up to 8’ WL
• Displacement (molded) up to 24’ and 40 ‘WL (vertical

summation of waterplanes)

• Displacement (molded) up to 24’ and 40 ‘WL (Longitudinal

summation of stations)

• Wetted surface
• Summary of results of Calculations

4’wl area 8’wl area 16’wl area 24’wl area 32’wl area 40’wl area Up to 4’wl Up to 8’wl Up to 24’ & 40 wl

• Disp. Up

to 24’wl

• Disp. Up

to 40’wl

• Disp. Up

to 16’wl

• Disp. Up

to 32’wl MTI MTI Wetted surface Summary

Red sheet will be studied in detail

• 1-6 Areas & properties (F.C.,

Ic, etc) of W.L

• 7-11 Displacement, ZB , and

XB up W.L., vertical integration.

• 12-15 Transverse station area,

longitudinal integration for displacement, ZB , and XB

• 16-18 Specific Feature (wetted

surface, MTI, etc.

• 19 Summary

23/06/2017 5 

1 1 2 3 12 1 2

2 2 3 The distance between the two stations 2 Simpson's 1st 3 2 1 2 3 2 2 2 1 3 4 3 2 .. 4 2 Symmetric m S S y y y y y y y y                        

2 2 3 3 3 4 5 6

Formulas for the remaining coefficents 2 2 3 the distance between the two stations 2 Simpson's 1st rule coeff.; 2 - Symmetric 3 2 2 3 1 2 1 2 ( from ) 3 3 3 3 2 2, 3 3

i

m m S S m S y m S h m S m               

2

2 2 3 3 h S    

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Illustration of Table 4: C1 Station FP-0 AP-10 (half station) C2 Half Ordinate copy from line drawing table ( 24’ WL). (notice at FP. Modification of half ordinate) C3 Simpson coefficient (Simpson rule 1) (1/2 because of half station) C4 = C3 x C2 (area function) displacement C5 = Arm (The distance between a station and station of 5 (Midship) C6 = C5 x Function of Longitudinal Moment with respect to Midship (or station 5) C7 = Arm (same as C5) C8 = C6 x C7 Function of Longitudinal moment of inertia with respect to Midship. C9.= [C2]3

• C10. Same as C3. (Simpson Coeff.)
• C11. = C9 x C10. Transverse moment of inertia of WL about its centerline

Table 5 is similar to Table 4, except the additional computation of appendage.

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Illustration of Table 8

For low WLs, their change is large. Therefore, it is first to use planimeter or other means to compute the half-areas of each stations up to No. 1 WL (8’ WL). C1. Station C2. Half area (ft2) of the given station C3.C3/(h/3) ( divided by h/3 is not meaningful, because it later multiplying by h/3) (h = 8’ the distance between the two neighboring WLs) C4.½ Simpson’s Coeff. C5. C4 x C3 C6.Arm distance between this station and station 5 (midship) C7 C5 x C6 f(M)

23/06/2017 8 Illustration of Table 9

C1. WL No. C2. f(V) Notice first row up to 8’. f(v) C3. Simpson’s coeff.

• C4. C2 x C3
• C5. Vertical Arm above the base

C6. C4 x C5. f(m) vertical moment w.r.t. the Baseline. * Notice up the data in the first row is related to displacement up to 8’

• WL. The Table just adding V)

23/06/2017 9 Illustration of Table 12

• C1. Station No.
• C2. under 8’ WL.

(From Table 8) C3. 8’ WL x 1 C4. 16’ WL x ¼ (SM 1 + 4 + 1) C5. 24’ WL x 1 C6. (C2 + C3 + C4 + C5) Function of Area of Stations C7. Arm (Distance between this station to midship) C8. C7 x C6 (Simpson rule)

• C9. C6*h/3

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4.3 Stability

A floating body reaches to an equilibrium state, if 1) its weight = the buoyancy 2) the line of action of these two forces become collinear. The equilibrium: stable, or unstable or neutrally stable.

• Stable equilibrium: if it is slightly displaced from its

equilibrium position and will return to that position.

• Unstable equilibrium: if it is slightly displaced form its

equilibrium position and tends to move farther away from this position.

• Neutral equilibrium: if it is displaced slightly from this

position and will remain in the new position.

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• Motion of a Ship:

6 degrees of freedom

• Surge
• Sway
• Heave
• Roll
• Pitch
• Yaw

Axis Translation Rotation x Longitudinal Surge Neutral S. Roll S. NS. US y Transverse Sway Neutral S. Pitch S. z Vertical Heave S. (for sub, N.S.) Yaw NS

Righting & Heeling Moments

A ship or a submarine is designed to float in the upright position.

• Righting Moment: exists at any angle of inclination where

the forces of weight and buoyancy act to move the ship toward the upright position.

• Heeling Moment: exists at any angle of inclination where

the forces of weight and buoyancy act to move the ship away from the upright position.

23/06/2017 12 G---Center of Gravity, B---Center of Buoyancy M--- Transverse Metacenter, to be defined later. If M is above G, we will have a righting moment, and if M is below G, then we have a heeling moment.

W.L

For a displacement ship, For submarines (immersed in water)

G B G

If B is above G, we have righting moment If B is below G, we have heeling moment

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Upsetting Forces (overturning moments)

• Beam wind, wave & current pressure
• Lifting a weight (when the ship is loading or unloading in

the harbor.)

• Offside weight (C.G is no longer at the center line)
• The loss of part of buoyancy due to damage (partially

flooded, C.B. is no longer at the center line)

• Turning
• Grounding

Longitudinal Equilibrium

For an undamaged (intact) ship, we are usually only interested in determining the ship’s draft and trim regarding the longitudinal equilibrium because the ship capsizing in the longitudinal direction is almost impossible. We only study the initial stability for the longitudinal equilibrium.

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Static Stability & Dynamical Stability

Static Stability: Studying the magnitude of the righting moment given the inclination (angle) of the ship*. Dynamic Stability: Calculating the amount of work done by the righting moment given the inclination of the ship. The study of dynamic Stability is based on the study of static stability.

• Static Stability

1) The initial stability (aka stability at small inclination) and, 2) the stability at large inclinations.

• The initial (or small angle) stability: studies the right

moments or right arm at small inclination angles.

• The stability at large inclination (angle): computes the right

moments (or right arms) as function of the inclination angle, up to a limit angle at which the ship may lose its stability (capsizes). Hence, the initial stability can be viewed as a special case of the latter.

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Initial stability

• Righting Arm: A symmetric ship is inclined at a small angle

dΦ. C.B has moved off the ship’s centerline as the result of the

• inclination. The distance between the action of buoyancy and

weight, GZ, is called righting arm.

• Transverse Metacenter: A vertical line through the C.B

intersects the original vertical centerline at point, M.

sin if 1 GZ GM d GMd d      ฀

Location of the Transverse Metacenter

Transverse metacentric height : the distance between the C.G. and M (GM). It is important as an index of transverse stability at small angles of inclination. GZ is positive, if the moment is righting moment. M should be above C.G, if GZ >0. If we know the location of M, we may find GM, and thus the righting arm GZ or righting moment can be determined given a small angle dΦ. How to determine the location of M?

23/06/2017 16 When a ship is inclined at small angle dΦ WoLo – Waterline (W.L) at upright position W1L1 – Inclined W.L Bo – C.B. at upright position, B1 – C.B. at inclined position

• The displacement (volume) of the ship

v1, v2 – The volume of the emerged and immersed g1, g2 – C.G. of the emerged and immersed wedge, respectively



Equivolume Inclination

(v1 =v2 ) If the ship is wall-sided with the range of inclinations of a small angle dΦ, then the volume v1 and v2 , of the two wedges between the two waterlines will be same. Thus, the displacements under the waterlines WoLo and W1L 1 will be same. This inclination is called equivolume inclination. Thus, the intersection of WoLo, and W1 L1 is at the longitudinal midsection. For most ships, while they may be wall-sided in the vicinity of WL near their midship section, they are not wall-sided near their sterns and bows. However, at a small angle of inclination, we may still approximately treat them as equivolume inclination.

23/06/2017 17 When a ship is at equivolume inclination, According to a theorem from mechanics, if one of the bodies constituting a system moves in a direction, the C.G. of the whole system moves in the same direction parallel to the shift of the C.G. of that body. The shift of the C.G. of the system and the shift of the C.G of the shifted body are in the inverse ratio of their weights.

1 2 1 1 2

, vg g B B v v v    

3 1 1 2 3 3 1 2

2 3 , tan( ) tan( ) 1 2 2 2 ( tan ) (2 ) tan , 2 3 3 3 the moment of inertia of W L w.r.t. the longitudinal axis

L x L L L x x

y dx B B I vg g B M d d vg g y y d y dx d y dx I y dx I                  

   

For a ship inclined at a small angle , the location of its transverse metacenter is approximately above its C.B. by , which is independent of . . . (Metacenter measured from keel ), or is

x M

d I d K M H   

.

the height of metacenter above the baseline. , where is the vertical coordinates of the C.B. The vertical distance between the metacenter & C.G,

x M B B x M G B G

I K.M. = H = +Z Z I GM H Z +Z Z      

23/06/2017 18 If we know the vertical position of the C.G., and the C.B., the righting arm at small angles of inclination, , and the righting moment is .

G B x B G x w B g

Z Z d I GZ GM d Z Z d I M Z Z d                             

Examples of computing KM

d B

3 2 2 3 2 2

) Rectangular cross section 1 , , 2 12 12 12 2 ) Triangular cross section 2 1 1 , , 3 12 2 6 2 6 3

B x x B B x x B

a d Z I LB LBd I B BM d B d KM BM Z d b d Z I LB LBd I B BM d B d KM BM Z d                       d B

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Natural frequency of Rolling of A Ship

2 2 2

Free vibration where is the inertia moment of the ship w.r.t. C.G. A large leads to a higher natural freq.

X w w X X

M GM t GM M M GM            

4.4Effects of free surfaces of liquids on the righting arm

pp81-83

• When a liquid tank in a ship is not full,

there is a free surface in this tank.

• The effect of the free surface of liquids
• n the initial stability of the ship is to

decrease the righting arm. For a small parallel angle inclination, the movement of C.G of liquid is

1 tan OL k

I G G d  

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• The increase in the heeling moment due to the movement
• f C.G. of liquid

tan 1 heeling F k F OL

M G G I d       

If there is no influence of free-surface liquids, the righting moment of the ship at a small angle dΦ is:

• x

w B g w

I M GM d Z Z d                     In the presence of a free-surface liquid, the righting moment is decreased due to a heeling moment of free-surface liquid. The reduced righting moment M’ is

• x
• l

F heeling w B g w

I I M M M d Z Z                     

The reduced metacentric height GM’:

OX F OL B g w

I I GM Z Z         

Comparing with the original GM, it is decreased by an amount,

.

OL F w

I   

The decrease can also be viewed as an increase in height

• f C.G. w.r.t. the baseline.

OL F g g w

I Z Z      

How to decrease IOL:

• Longitudinal subdivision: reduce the width b, and thus reduces

Anti rolling tank

3 OL

I b l 

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4.5 Effects of a suspended weight on the righting arm

• When a ship inclines at a small

angle dΦ, the suspended object moves transversely

• Transverse movement of the weight

= h dΦ , where h is the distance between the suspended weight and the hanging point

• The increase in the heeling moment

due to the transverse movement

heeling

M w h d    In the presence of a suspended object, the righting moment & righting arm are decreased due to a heeling moment of the suspended object. The reduced righting moment M’ & metacentric height GM’ are:

• x

heeling w B g w

• x

B g w w

I w M M M d Z Z h I w w GM GM h Z Z h                                

In other words, the C.G of a suspended object is actually at its suspended point

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Because the suspension weights & liquid with free surface tend to decrease the righting arm, or decrease the initial stability, we should avoid them.

• 1. Filling the liquid tank (in full) to get rid of the

free surface. (creating a expandable volume)

• 2. Make the inertial moment of the free surface as

small as possible by adding the separation longitudinal plates (bulkhead).

• 3. Fasten the weights to prevent them from moving

transversely.

4.6 The Inclining Experiment (Test)

Purpose

• 1. To obtain the vertical position of C.G

(Center of Gravity) of the ship.

• 2. It is required by “International convention
• n Safety of Life at Sea.” (Every

passenger or cargo vessel newly built or rebuilt)

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4.6 The Inclining Experiment (Continue) Basic Principle

M: Transverse Metacenter (A vertical line through the C.B intersects the original vertical centerline at point, M) Due to the movement of weights, the heeling moment is

heeling

M wh 

where w is the total weight of the moving objects and h is the moving distance.

4.6 The Inclining Experiment (Continue)

The shift of the center of gravity is where W is the total weight of the ship. The righting moment = The heeling moment

1

wh GG W 

 

1

tan cot( ) tan( ) wh GM W wh GM GG W          

• 1. w and h are recorded and hence known.

2. is measured by a pendulum known as stabilograph.

• 3. The total weight W can be determined given the draft T. (at

FP, AP & midship, usually only a very small trim is allowed.)

• 4. Thus GM can be calculated,

 

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4.6 The Inclining Experiment (Continue) ,

x M g M B

I GM H Z H Z     

The metacenter height and vertical coordinate of C.B have been calculated. Thus, C.G. can be obtained.

g M

Z H GM  

Obtaining the longitudinal position of the gravity center of a ship will be explained in section 4.8.

4.6 The Inclining Experiment (Continue)

.

• 1. The experiment should be carried out in calm water & nice weather. No

wind, no heavy rain, no tides.

• 2. It is essential that the ship be free to incline (mooring ropes should be as

slack as possible, but be careful.)

• 3. All weights capable of moving transversely should be locked in position

and there should be no loose fluids in tanks.

• 4. The ship in inclining test should be as near completion as possible.
• 5. Keep as few people on board as possible.
• 6. The angle of inclination should be small enough with the range of validity
• f the theory.
• 7. The ship in experiment should not have a large trim.

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4.7 Effect of Ship’s Geometry on Stability

Transverse metacenter height GM = BM – (ZG –ZB)

3 2 2 1 1 1

( ) where dpends on waterplane. 2

x g B x B B x x

I GM Z Z I C LB C B B C C C LBT C T T I d dB dT I B T                        

4.7 (Continue)

a) Increase only: 2 ( increases) b) Decrease T only: ( decreases) c) Change B & T but keep fixed:

x B x x x x x

I d dB B C LBT I B I d dT I T dB dT B T I d I                                                    3 dB B 

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• Conclusion: to increase GM ( Transverse metacenter

height)

• 1. increasing the beam, B
• 2. decreasing the draft, T
• 3. lowering C.G (ZG)
• 4. increasing the freeboard will increase the ZG, but will

improve the stability at large inclination angle.

• 5. Tumble home or flare will have effects on the stability at

large inclination angle.

• 6. Bilge keels, fin stabilizers, gyroscopic stabilizers, anti-

rolling tank also improve the stability (at pp248-252).

4.7 (Continue)

Suitable metacenter height

• It should be large enough to satisfy the requirement of

rules.

• Usually under full load condition, GM~0.04B.
• However, too large GM will result in a very small rolling
• period. Higher rolling frequency will cause the crew or

passenger uncomfortable. This also should be avoided. (see page 37 of this notes)

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4.8 Longitudinal Inclination

Longitudinal Metacenter: Similar to the definition of the transverse meta center, when a ship is inclined longitudinally at a small angle, A vertical line through the center of buoyancy intersects the vertical line through (before the ship is inclined) at .

1

B B

L

M

• The Location of the Longitudinal Metacenter

For a small angle inclination, volumes of forward wedge immersed in water and backward wedge emerged out of water are:

1 2 1 2

(2 ) ( tan ) where is the half breadth. (2 ) ( tan ) , . Thus, 2 2 , which indicates: moment of area forward of = moment of area after . is the cente

l L l l L l

v y x dx y v y x dx v v v yxdx yxdx F F F  

 

      

   

r of (mass) gravity of waterline , & is called

• f

. Therefore, for equal volume longitudinal inclination the new waterline always passes through the (C.F W L W L center of flotation center of flotation ).

23/06/2017 28

• Location of the Longitudinal Metacenter

Using the same argument used in obtaining transverse metacenter.

1 1 2 1 2 2 2 1

/ , (2 ) ( tan ) 2 tan tan 2 2 tan is the moment of inertia with respect to the transverse axis passing the center of flotation. t

l L l l FC L l FC

B B vg g vg g y x xdx yx xdx yx dx yx dx I I B B B M    

 

               

   

an , . .

FC FC FC ML B B L B g

I B M I I H B M Z Z GM Z Z            

• Location of the Longitudinal Metacenter

2 0, 0,

Usually Floatation Center (C.F) of a waterplane is not at the midship, , where is the moment of inertia w.r.t. the transverse axis at midship (or station 5) and is the distance from F

FC T T

I I Ax I x   .C. to the midship.

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• Moment to Alter Trim One Inch (MTI)

MTI: (moment to alter (change) the ship’s trim per inch) at each waterline (or draft) is an important quantity. We may use the longitudinal metacenter to predict MTI

• MTI ( a function of draft)

Due to the movement of a weight, assume that the ship as 1” trim, and floats at waterline W.L.,

   

1 1 1

1" 1 tan , where is in feet. 12 Due to the movement of the weight, moves to , , tan tan tan tan 1 12

w L L G FC w L G w B G FC w B G

L L L G G M w h G G G G G M HM Z I M HM Z Z Z I Z Z L                                              

23/06/2017 30

• MTI ( a function of draft)
• If the longitudinal inclination is small, MTI can be used to find
• ut the longitudinal position of gravity center ( ).

3

1 , 12 12 64 lb/ft , Long Ton = 2240 lb, MTI (ton-ft) 420

FC FC w FC G B w FC w

I I I Z Z M L L I L              

1 G

X

1 1 1

Trim tan tan , Since is in the same vertical line as . under ,

F A FC FC FC B G G B FC G B B

T T T L L L I I I T G G Z Z Z Z L G C B W L I T X X G G X L                             ฀