OVERALL STABILITY 4.1 External Forces Acting on a Vessel In Chapter 4 we will study five areas: 1. The concept of a ship s Righting Moment (RM), the chief measure of stability. 2. KG and TCG changes and their effects on RM. 3. How Stability is effected by Damage to the Hull using the Added Weight method. 4. Effects of a Free Surface. 5. Effects of Negative GM on ship stability.
4.2 Internal Righting Moment EXTERNAL FORCES cause a vessel to heel. Recall Force x Distance = Moment External Moment can be caused by wind pushing on one side of the vessel and water resisting the motion on the other side. Each distributed force can be resolved into a resultant force vector. The wind acts above the waterline and the water resistance acts below the waterline.
Internal Righting Moment M T External upsetting force f D s G F Z Righting Arm f WL f B F B Water resistance C L
Internal Righting Moment The two forces create a couple because they are equal in magnitude, opposite in direction, and not aligned. The couple causes rotation or heeling. The vessel will continue to rotate until it returns to Static Equilibrium (i.e. an Internal Moment is created which is equal in magnitude and opposite in direction). Giving M=0.
Internal Righting Moment Internal Forces create a Righting Moment to counter the Upsetting Moment of the External Forces. The two internal forces are the weight of the vessel ( s ) and the resultant buoyant force (F B ).
Internal Righting Moment The perpendicular distance between the Weight and the Buoyancy Force vectors is defined as the RIGHTING ARM (GZ). The moment created by the resultant Weight and the resultant Force of Buoyancy is defined as the RIGHTING MOMENT (RM). It may be calculated by: RM = GZ = s GZ F B
Internal Righting Moment Where: RM is the internal righting moment of the ship in ft-lt. s F B is displacement of the ship in LT. is the magnitude of the resultant buoyant force in LT. GZ is the righting arm in feet.
A ship in static equilibrium is affected by outside forces that will alter its state of equilibrium. M T Wind Water Resistance The forces of wind- and the opposing force of the water below the waterline- will cause an external moment couple about the ship s center of flotation.
The ship reacts to this external moment couple by pivoting about F, causing a shift in the center of buoyancy. M T Wind B Water Resistance The center of buoyancy will shift because the submerged volume will change. Note that there is no change in weight or it s distribution so there is NO change in the location of G!
Because the location of B changes, the location of where the F B is applied also changes. Because G does not move, the location of the Δs force does not change. s M T B F B The displacement force and the buoyant for are no longer aligned. The heeling over causes the creation of an internal moment couple.
The external moment couple causes the creation of the internal moment couple to oppose it. Wind s M T F F B B Water Resistance As a result, the ship is now back into equilibrium, even as it heels over due to the wind force.
We are concerned with the created internal moment caused by the offsetting of the ship s weight and the buoyant force. Ds M T Z f B F B The offset distance of the applied forces, GZ, is called the MOMENT ARM. The length of this moment arm is a function of the heeling angle, φ.
Remember that a moment is created when a force acts at a distance from a given point. In the case of the created internal moment couple, we have the two force, Ds and F B, acting over the distance GZ. The created moment is called the internal RM = GZD s = GZF B
This illustrates just one potential moment arm based upon one particular angle of φ. There are an infinite number of angles possible, therefore, an infinite number of moment arms that vary with the degree of heel, φ. Ds M T Z f B F B If we can plot the heeling angle f versus the created moment arm GZ, we can create the Intact Statical Stability Curve.
4.3 Curve of Intact Statical Stability Curve of Intact Statical Stability or The Righting Arm Curve Shows the Heeling Angle ( ) versus the righting arm (GZ). Assumes the vessel is heeled over quasistatically in calm water (i.e. external moments are applied in infinitely small steps).
This is a typical curve. Notice that it plots the angle of heel on the x-axis and the righting arm on the y-axis. The curve is in both the 1st and 3rd quadrants (the 3rd shows a heel to port). Typically only the curve showing a heel to starboard is shown as it is symmetrical.
Measure of Overall Stability Curve of Statical Stability Righting Arm - GZ -(feet) Range of Stability Slope is a measure of tenderness or stiffness. Dynamical Stability Maximum Righting Arm Angle of Maximum Righting Arm Angles of Inclination: (Degrees)
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle The above chart plots the data presented in the text on p. 4-6 an 4-7.
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle With φ at 0 degrees, the moment arm is also is 0. The buoyant force and the ship s weight are aligned. No moment is created.
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle As the angle of heel increases, the moment arm also increases. At 25 degrees, shown here, GZ is 2.5ft.
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle As the angle increases, the moment arm increases to a maximum here it is 4ft. As φ increases beyond this point the moment arm begins to decrease and the ship becomes in danger of capsizing
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle...Remember, the internal moment couple created here is in response to the external couple created by outside forces. At GZ max the ship is creating its maximum internal moment. If the external moment is greater than the internal moment, then the ship will continue to heel over until capsized.
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle The angle of heel continues to increase, but the moment arm GZ, and thus the internal moment couple, decreases.
Intact Statical Stability Moment Arm GZ 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 25 50 75 85 Heeling Angle The angle has now increased to the point that G and B are now aligned again, but not in a good way. GZ is now at 0 and no internal moment couple is present. Beyond this point the ship is officially capsized, unable to right itself.
Curve of Intact Statical Stability Caveats! Predictions made by the Curves of Intact Statical Stability are not accurate for dynamic seaways because additional external forces and momentum are not included in the analysis. Added Mass However, it is a simple, useful tool for comparison and has been used to develop both intact and damaged stability criterion for the US Navy.
Curve of Intact Statical Stability Typical Curve of Intact Statical Stability Vessel is upright when no external forces are applied and the Center of Gravity is assumed on the centerline. (Hydrostatics) As an external force is applied, the vessel heels over causing the Center of Buoyancy to move off the centerline. The Righting Arm (GZ) is no longer zero.
Curve of Intact Statical Stability Typical Curve of Intact Statical Stability (cont.) As the angle of heel increases, the Center of Buoyancy moves farther and farther outboard (increasing the Righting Arm). The max Righting Arm will happen when the Center of Buoyancy is the furthest from the CG. This is max stability. If the vessel continues to heel, the Center of Buoyancy will move back towards the CG and the Righting Arm will decrease.
Curve of Intact Statical Stability Typical Curve of Intact Statical Stability (cont.) Since stability is a function of displacement, there is a different curve for each displacement and KG. These are called the Cross Curves.
For all ships, there exists the CROSS CURVES OF STABILITY. Like the Curves of Form, they are a series of curves presented on a common axis. The x-axis is the ship s displacement, Δ s, in LT The y-axis is the righting arm, GZ, in ft A series of curves are presented, each representing a different angle of heel f By plotting the data from the Cross Curves of Stability for a given displacement, you can create an Intact Statical Stability Curve.
In the Cross Curves of Stability, the data is presented assuming that: KG = 0 (on the keel) This is, of course, not realistic. It is done this way so that the curves may be generalized for all drafts. Once the curve data is recorded and plotted, a sine correction factor must be applied, shifting the KG to its correct position in order to get the TRUE MOMENT RIGHTING ARM VALUE.
Cross Curves Example Righting Arm (feet) 5 30 degrees heel 2.5 0 10 degrees heel 1000 2000 3000 Displacement (LT) At 2000 LT, the ship Has a RA of 2.5 @10 o Heel and 5 @30 o
Curve of Intact Statical Stability / Righting Arm Curve Assumes: Quasi-static conditions Given Displacement Given KG Cross Curves of Stability Since M T moves as a function of φ, Righting Arms are calculated for each φ at regular intervals Assumes a value of KG
4.4 Measure of Overall Stability From the Curves of Intact Stability the following Measures of Overall Stability can be made: Range of Stability Maximum Righting Moment Angle of Maximum Righting Moment Dynamical Stability Measure of Tenderness or Stiffness
Measure of Overall Stability Range of Stability The range of angles for which there exists a positive righting moment. The greater the range of stability, the less likely the ship will capsize. If the ship is heeled to any angle in the range of stability, the ship will exhibit an internal righting moment that will right the ship if the external moment ceases.
Measure of Overall Stability Maximum Righting Moment The largest Static Moment the ship can produce. Calculated by multiplying the displacement of the vessel times the maximum Righting Arm. The larger the Maximum Righting Moment, the less likely the vessel is to capsize.
Measure of Overall Stability Angle of Maximum Righting Arm The angle of inclination where the maximum Righting Arm occurs. Beyond this angle, the Righting Arm decreases. It is desirable to have a larger maximum angle so that at large angles of heel in a rolling ship the righting moment will continue to increase.
Measure of Overall Stability Dynamical Stability: The work done by quasi-statically rolling the ship through its range of stability to the capsizing angle. Can be calculated by the equation: D s GZ d. This is equal to the product of the ship s displacement with the area under the Curve of Intact Statical Stability. Not shown directly by the Curve of Intact Statical Stability. Does not account for the actual dynamics, because it neglects the impact of waves and momentum.
Measure of Overall Stability Measure of Tenderness or Stiffness The initial slope of the intact statical stability curve indicates the rate at which a righting arm is developed as the ship is heeled over. This slope is GM! A steep initial slope indicates the rapid development of a righting arm and the vessel is said to be stiff. Stiff vessels have short roll periods and react strongly to external heeling moments. A small initial slope indicates the slower development of a righting arm and the vessel is said to be tender. Tender vessel have longer roll periods and react sluggishly to external heeling moments.
Example: Plot the Intact Statical Stability Curve for an FFG-7 displacing 5000LT Step #1. From the Cross Curves of Form, find the 5000LT displacement value on the x-axis. Step #2. Record the righting arm value for each curve, from φ = 0 to 80 degrees Step #3. Draw the curve, using φ as x-axis, and GZ as y-axis
Intact Statical Stability Curve for FFG-7 @ s = 5000LT f GZ 0 0.00 5 2.00 10 3.80 15 5.80 20 7.75 25 9.75 30 11.75 35 13.30 40 14.75 45 16.10 50 17.20 55 18.00 60 18.60 65 19.00 70 19.30 80 19.50 Moment arm GZ 25 20 15 10 5 0 Intact Statical Stability, FFG-7 0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 Heeling Angle But a correction must still be made!!
Example Problem The Statical Stability curve applies to a ship with D=3600LT. 5 4 Curve of Intact Statical Sta bility The ship is being pulled sideways into a 10 list by a tug attached to the ship 10ft above the Waterline. How much force is the tug applying to the tow line? Righting Arm (GZ)(ft) 3 2 1 0-10 0 10 20 30 40 50 60 70 80 90 100-1 -2 Angle of Heel (Degrees)
Example Answer F=10 F Tug F G D B F B 10ft Water Resistance RM=GZΔ=1.2ft 3600LT=4320ft-LT Upsetting Moment from Tug=F Tug 10ft=RM (in static equilibrium) F Tug =4320ft-LT/10ft=432LT
4.5 Effect of a Vertical Shift in the Center of Gravity on the Righting Arm In the Cross Curves of Stability, the data is presented assuming that: KG = 0 (on the keel) This is, of course, not realistic. It is done this way so that the curves may be generalized for all drafts. Once the curve data is recorded and plotted, a sine correction factor must be applied,shifting the KG to its correct position in order to get the TRUE MOMENT RIGHTING ARM VALUE. Must Apply a Sine Correction if: Using the Curve of Intact Statical Stability to correct for G not being located at K Correcting the Curve of Intact Statical Stability for vertical movements of G
The external moment couple causes the creation of the internal moment couple to oppose it. Wind s M T B Water Resistance F B External Moment Couple = Internal Moment Couple
When the ship heels over, the center of buoyancy, B, shifts. The shift creates a distance or moment arm. M T f Z 0 B 1 G 0 Z 0 = Moment Arm
For values taken from the Cross Curves of Stability, G 0 is at the keel... M T f B 1 Z 0 G 0 Z 0 = Moment Arm This value is recorded as G 0 Z 0, the Initial Moment Arm.
The KG value for the ship is given this is the ACTUAL G position from the keel... M T f B 1 KG forms a similar triangle that gives the value for the SINE correction Z 0
Sin f = opp hyp opp =correction factor hyp = KG Sine Correction factor = KG Sin f
M T f B 1 Z 0 Sin Correction = KG Sin f
M T f Z v B 1 Z 0 G v Z v = G 0 Z 0 - KG sinf
Effect of a Vertical Shift in the Center of Gravity on the Righting Arm As KG rises the righting arm (GZ) decreases. This change in GZ can be found from: Where: G v Z v = G 0 Z 0 - G 0 G v sin F G v is the final vertical location of the center of gravity. G 0 is the initial location of KG. Typically, G 0 G V =KG final
Effect of a Vertical Shift in the Center of Gravity on the Righting Arm Sine Correction: D s F M T G v Z v = G 0 Z 0 - G 0 G v sin F G Z G o, Z o =initial locations G v, Z v =final positions G F P 0 Z 0 W L B 0 B F b
Effect of Increased Displacement on the Righting Arm A higher displacement should increase the Righting Moment as RM= Displacement * RA But, if the added weight is high, then the KG increase could cause a reduction in GZ Weight added low down usually increases stability
Effect of a Vertical Shift in the Center of Gravity on the Righting Arm
4.6 Stability Change for Transverse Shift in CG So far we have only considered the case where the Center of Gravity is on the centerline (TCG=0). The center of gravity may be moved off the centerline by weight additions, removals, or shifts such as cargo loading, ordnance firing, and movement of crew.
Stability Change for Transverse Shift in the CG G v G v G t cos F F G t F M T Port Starboard Ds W 1 F L1 G v F G t B 1 Z V Z t F b
The red line indicates the COSINE Correction factor for a transverse change in G. f Z v G T Z T Note that G v G T is the TCG value and is the hypotenuse of this correction triangle... Cosine Corr = G v G T cosf
The final moment arm, G T Z T, is the correct moment arm f Z v G T Z T G T Z T = G v Z v - G v G T cosf
Stability Change for Transverse Shift in the CG The new righting arm created by a shift in TCG may be computed at each angle from the Cosine Correction: G t Z t = G v Z v -G v G t cos F...Typically, G V G t =TCG final
Stability Change for Transverse Shift in the CG The new righting arm (G t Z t ) created due to the shift in the transverse center of gravity is either shorter or longer than the righting arm created if TCG=0. The range of stability has decreased on the side that the transverse center of gravity has shifted to but has increased on the side it shifted from.
Combining both the vertical and horizontal corrections by substituting for G v Z v you can get a final general formula for determining moment arms: G T Z T = G 0 Z 0 - KG sinf - G v G T cosf
Example Curves Correction Statical Stability Curve and Corrections 15 Righting Arm from Cross Curves Righting Arm (GZ)(ft) 10 5 0-140 -5-10 -15-130 -120-110 -100-90 -80-70 -60-50 With Sine Correction With Cosine Correction -40-30 -20-10 0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 Angle of Heel (degrees)
Various Righting Arm Conditions D G B F B F=0 D G Z B F=30 F B D G Z B F B F=RA Max D G B F B F=Capsize Angle B F B D G F= >Capsize Angle
Example Problem FFG-7, with draft 13.5ft, which would otherwise be on an even keel, is heeling 15 to starboard in a gale. KG is 17ft. What is the Righting Moment?
Example Answer RM=GZΔ G V Z V =G 0 Z 0 -G 0 G V sinf From Curves of Form: Draft of 13.5ft-> Δ =100 30LT=3000LT From Cross Curves for Δ =3000LT, φ=15, G 0 Z 0 =6ft G 0 G V =KG=17ft G V Z V =6ft-17ft sin(15 )=1.6ft RM=1.6ft 3000LT=4800ft-LT
Example Problem FFG-7, with draft 13.5ft, which would otherwise be on an even keel, is heeling 15 to port in a gale. KG is 17ft. While in this condition, 50LTs of unsecured stores shift from 20 ft starboard of centerline to 20ft port of centerline. What is the Righting Moment? What would the Righting Moment be if the weight had shifted the other way?
RM=GZ Δ Example Answer G f Z f =G 0 Z 0 -G 0 G V sin φ -G V G t cosφ From Curves of Form: Draft of 13.5ft-> Δ =100 30LT=3000LT From Cross Curves for Δ =3000LT, φ =(-)15, G 0 Z 0 =(-)6ft G 0 G V =KG=17ft G V G t = TCG f =(TCG 0 Δ 0 +STcg a w a -STcg r w r )/ Δ f =(0ft 3000LT+(-)40ft 50LT)/3000LT=(-).67ft G f Z f =(-)6ft-17ft sin(-15 )-(-.67ft) cos(-15 )=(-).953ft RM=(-).953ft 3000LT=(-)2860ft-LT vice (-)4800ft-LT in the case without the weight shift (~40% reduction) G f Z f =(-)6ft-17ft sin(-15 )-(+.67ft) cos(-15 )=(-)2.247ft RM=(-)2.247ft 3000LT=(-)6741ft-LT vice (-)4800ft-LT in the case without the weight shift (~40% improvement)
4.7 How Does a Ship Sink? 3 of the 6 Degrees of Freedom can sink a ship Foundering(heave): Ship fills up with water from the bottom up and simply sinks on a relatively even keel (Loss of Buoyancy) Overwhelm and Capsize: Ship still floats and is stable but has insufficient Righting Arm and Dynamical Stability for weather and sea conditions, which eventually roll the ship past range of stability Plunging: Pitch angle becomes excessive causing the ship to sink bow or stern first Progressive Flooding: Excessive list and/or trim angle and/or failure of bulkheads adjacent to flooded compartments resulting in one or more of the loss modes above.
Damage Stability Flooding - Water ingression such that the vessel has sinkage and trim but no list. May be intentional. Damage - Water ingression such that the vessel has sinkage, trim and list.
When a vessel is damaged, creating a a gap or hole in the hull, water will breech the ship. This results in: Increase in draft Change in trim Permanent angle of list The result of this flooding can be determined two ways: Lost Buoyancy Method Added Weight Method
Consider a vessel that has been damaged such that a portion of the bottom is now open to the sea... The vessel s draft will increase because an amount of the buoyancy was lost...
Lost buoyancy considers the amount of buoyancy lost as a result of the hole, and determines the value based upon the change in parallel sinkage that results. Original draft The change in the draft reflects the amount of buoyancy lost. The ship sinks until the available submerged volume is again equal to the ship s displacement
Lost Buoyancy Method Analyzes damage by changes in buoyancy versus changes in the Center of Gravity. Premise is that the ship s CG does not move. Since weight does not change, total buoyant volume must also be constant. Therefore, the ship makes up any lost buoyancy volume from damage by listing, trimming, and draft changes.
The Added Weight Method considers the resulting flooding as though it was a weight added to the ship. This is the method that will be used in this course. Original draft A flooded compartment does not fill completely with water, however. Compartments contain equipment, furniture, structural components, and cargo. A correction factor must be added to the volume of the compartment to accurately reflect conditions...
This correction factor is called: PERMEABILITY = AVAILABLE VOLUME TOTAL VOLUME Some typical factors are: Watertight compartment (warship) 97% Watertight compartment (merchant) 95% Accommodation spaces 95% Machinery spaces 85% Dry cargo spaces 70% Bunkers, stores, cargo holds 60%
Added Weight Method The One We Will Use Damaged Ship Modeled as Undamaged But with Water- Filled Spaces. Average Distances of Space from Keel, Midships, and Centerline Known & Water Density Known. Therefore Can Solve for Shifts in G as a Weight Addition Problem
Added Weight Method Independently Solve for Damaged Condition KG TCG Draft and Trim Must know compartment contents to find Total of (Water Weight) Added. This involves a Permeability factor.
Permeability Compartments are rarely 100% flooded during damage, due to trapped air, equipment, etc. Ratio of volume occupied by water to the total gross volume is defined as permeability. Permeability = Volume Available for Flooding Total Gross Volume Permeability is always < or = to 100%!
Damage Stability Design Criteria Guiding rules for vessel design. Note that criteria used in static analysis will neglect the impact of dynamic forces such as wind and waves.
Damage Stability Design Criteria Three Main Criteria MARGIN LINE LIST EXTENT OF DAMAGE TO HULL
MARGIN LINE LIMIT Highest permissible location of any damaged waterplane. Must be at least 3 inches (0.075 m) below top of the bulkhead deck at the side.
LIST LIMIT Heel by damage 20 degrees. Naval machinery to operate indefinitely at a permanent list 15 degrees (most will function up to ~25 degrees for a few hours). Assumes personnel can continue damage control efforts effectively at a permanent list of 20 degrees. Ship must possess adequate stability against weather to be towed when at 20 degree list.
EXTENT OF DAMAGE TO THE HULL LIMIT 100 ft LOA: must withstand flooding in one space. 100-300 ft LOA: flooding in two adjacent compartments. Warships, troop transports and hospital ships over 300 ft LOA: hull opening up to 15 % of Lpp. Others 300 ft: hull opening up to 12.5% of Lpp.
Foundering and Plunging A vessel as result of damage or other events can be lost several ways: Insufficient transverse stability. It rolls over. (Could be static or dynamic.) Insufficient longitudinal stability. Plunging If insufficient buoyancy. It sinks. Foundering
Example Problem An FFG-7 with a draft of 13.5ft and a KG of 19ft on an even keel inport sails into the North Atlantic during Winter. While there, topside becomes coated with a 6in thick coating of ice of density of 55lb/ft³. The topside area covered is 20,500ft² and has a Kg of 40ft. In this condition, a space heater in CIC shorts generating a fire which is only extinguished by completely filling the 97% permeable 40ft 40ft 10ft space with firefighting (sea) water. The space is centered 45ft above the keel and 2.5ft port of centerline. What is the Righting Moment for a 15 port list and how could the resulting problem have been prevented?
Example Answer w ice =ρgv=55lb/ft³.5ft 20,500ft² 1LT/2240lb =252LT(@Kg=40ft) w ffwater = ρ gv=64lb/ft³ 40ft 40ft 10ft.97 1LT/2240lb =443LT(@Kg=45ft) Δ(Curves of Form[T=13.5ft])=100 30LT=3000LT KG f =(KG 0 Δ 0 +Kg a w a -Kg r w r )/ Δ f KG f =(19ft 3000LT+40ft 252LT+45ft 443LT) /(3000LT+252LT+443LT) KG f =23.5ft TCG f =(TCG 0 Δ 0 +Tcg a w a -Tcg r w r )/ Δ f TCG f =(0ft 3000LT+0ft 252LT+(-)2.5ft 443LT) /(3695LT) TCG f =(-)0.3ft G 0 Z 0 (Cross Curves[Δ =3695LT; φ =(-)15 ])=(-)6ft G f Z f =G 0 Z 0 -KG f sinφ-tcg f cosf G f Z f =(-)6ft-23.5ft sin(-15 )-(-.3ft) cos(-15 )=(+).372ft
Example Answer R.M.=Δ G f Z f =3695LT 0.372ft=(+)1375ft-LT to port for a port list: The ship capsizes! KM t (Curves of Form[Δ=3695LT;T=15.25ft])=112*.2ft=22.4ft (GM t =KM t -KG f =22.4ft-23.5ft=(-)1.1ft; Stable?) Center of Gravity is above Metacenter; ship rolls to port due to offset of flooded compartment and capsizes. Prevent by keeping topside clear of ice and dewatering fire spaces as soon as possible.
4.8 Free Surface Correction (Small Angles of Heel) Free Surface - A fluid that moves freely. Fluid Shift is a weight and causes the CG to shift in both the vertical and horizontal directions. Vertical shift is small for small angles and is usually ignored. Horizontal shift always causes a reduction in the righting arm (GZ).
Free Surface Correction Free Surface Correction (FSC) The distance the center of gravity would have to rise to cause a reduction in the righting arm equivalent to that caused by the actual transverse shift. "Virtual" center of gravity (G v ) The effective position of this new VCG. Effective Metacentric Height (GM eff ) The distance from the virtual center of gravity (G v ) to the metacenter. Note: Dynamic effects are neglected.
Free Surface Effect Static effects for small angles (F<=7 ) Effective g for tank is above tank g analogous to relationship between M and B M T g eff B 0 g 0 B f g f
Free Surface Correction The Big Picture M T GM eff G v F F FSC G B G 1 Z Z 1 F WL 1 WL g g 1 B 1. K
Free Surface Effect The new, effective VCG is G v, so a sine correction is applied to get the statical stability curve G 1 Z 1 = G t Z t - GG v sin f or G 1 Z 1 = G t Z t - FSC sin f
Free Surface Correction The free surface correction to GM for small angle hydrostatics is: FSC = t s i t s where: t is the density of the fluid in the tank in lb s 2 /ft 4 s is the density of the water the ship is floating in lb s 2 /ft 4 i t is the transverse moment of area of the tank's free surface area in ft 4. s is the underwater volume of the ship in ft 3.
Free Surface Correction i t is calculated for a rectangular tank as: The dimensions are for the free surface! i t = Tank (L) (B)3 X 12 L C L Y B
Effect on Ship G and Stability GZ eff =G 0 Z 0 -G 0 G v sinφ-g v G t cos φ -FSCsin φ Calculation of KG, etc. is already accounted for in this equation Free Surface Correction (FSC) already accounts for size of ship. GM eff =GM-FSC=KM-KG-FSC A large FSC has exactly the same effects on list and stability as a higher KG.
How do we minimize adverse effects of free surface effect? Compartmentalization Pocketing (Keep tanks >95% full) Empty Tanks Compensated Fuel Oil Tanks Dewater quickly after a casualty - flooding or fire
4.9 Metacentric Height Recall that Overall Stability is measured by: Range of Stability Dynamical Stability Maximum righting moment The angle at which the maximum righting moment occurs.
Initial Slope of the Curve of Intact Stability At small angles, a right triangle is formed between G, Z, and M. The righting arm may be computed: GZ = GM sin As 0, if the angle is given in radians the equation becomes: GZ = GM
Initial Slope of the Curve of Intact Stability Metacentric height can then be found from the initial slope of the Curve of Intact Statical Stability: GM = GZ sin = GZ (radians) GM = GZ (if = 1 radian) (for smallangles)
Initial Slope of the Curve of Intact Stability To find the slope either: Find the change in the y-axis over a given change in the x-axis. Draw a straight line with the initial slope and read the value of GZ at an angle of 57.3 degrees (i.e. one radian).
Metacentric Height LET S EXAMINE EACH GM CONDITION GM Positive (G < M) GM Zero (Neutral Stability) (G = M) GM Negative (G > M)
Positive Stability Metacentric Height
Neutral Stability Metacentric Height
Negative Stability Metacentric Height
Metacentric Height SUMMARIZING GM CONDITIONS GM Positive = Positive Stability (M > G) GM Zero = Neutral Stability (M = G) GM Negative = Negative Stability (M < G) Metacentric Height only a good indicator of stability over small angles. GM is initial slope of Curve Intact Stability
Stability Status Stability Adequate Margin Inadequate Adequate Status 1 Status 3 Weight Margin Inadequate Status 4 Status 2
Example Problem An FFG-7 with a draft of 13.5ft and a KG of 17ft on an even keel inport goes to sea. A space heater in CIC shorts generating a fire which is extinguished by completely filling the 97% permeable 40ft 40ft 10ft space with firefighting (sea) water. The flooded volume is centered 45ft above the keel and 2.5ft starboard of centerline. 1. What is the equilibrium list angle in this condition? 2. A large wave hits and forces the ship to a temporary 15 starboard list. What is the Righting Moment? 3. The CIC overhead, weakened by the heat of the fire, is blown off by a gale force wind, making the compartment now a free surface. What is the equilibrium list angle and Righting Moment for a temporary 15 starboard list?
Example Answer w ffwater =ρgv=64lb/ft³ 40ft 40ft 10ft.97 1LT/2240lb =443LT(@Kg=45ft) Δ(Curves of Form[T=13.5ft]) =100 30LT=3000LT KG f =(KG 0 Δ 0 +Kg a w a -Kg r w r )/ Δ f KG f =(17ft 3000LT+45ft 443LT) /(3000LT+443LT) KG f =20.6ft TCG f =(TCG 0 Δ 0 +Tcg a w a -Tcg r w r )/ Δ f TCG f =(0ft 3000LT+2.5ft 443LT) /(3443LT) TCG f =0.32ft
Example Answer KM t (Curves of Form[Δ =3443LT;T=14.6ft]) =114.2ft=22.8ft GM t =KM t -KG f =22.8ft-20.6ft=2.2ft tan(φ)=tcg f /GM t =0.32ft/2.2ft; φ =8.3 G 0 Z 0 (Cross Curves[Δ =3443LT; φ =15 ])=6ft G f Z f =G 0 Z 0 -KG f sin φ -TCG f cos φ G f Z f =6ft-20.6ft sin(15 )-(.32ft) cos(15 )=0.36ft R.M.= Δ G f Z f =3443LT 0.36ft=1240ft-LT
Example Answer CIC Overhead Blown Off: i t =lb³/12=40ft (40ft)³/12=213,333ft 4 V S =Δ/(ρg)=3443LT 2240lb/LT/(64lb/ft³)=120,505ft³ FSC=(ρ t i t )/(ρ S V S )=i t /V S =1.77ft (ρ t =ρ S ) GM eff =KM t -KG-FSC=22.8ft-20.6ft-1.77ft=0.43ft tan(φ)=tcg f /GM eff =0.32ft/0.43ft; f=36.7 (vice 8.3 ) G f Z f =G 0 Z 0 -KG f sinφ-tcg f cos φ -FSCsin φ G f Z f =6ft-20.6ft sin(15 )-(.32ft) cos(15 )-1.77ft sin(15 )=(-)0.1ft R.M.= Δ G f Z f =3443LT (-)0.1ft=(-)344.3ft-LT(vice +1240ft-LT) At 15, ship lists starboard but wants to list further starboard to reach 36.7
Example Problem Below are body plan views of three proposals for outriggers. Sketch the respective curves of Intact Statical Stability and comment on the stability and ride characteristics for each option. G G G
M Example Answer G G M GM Statical GZ Stability F StaticalGZ Stability F StaticalGZ Stability F Positively stable: Very stiff roll characteristic Unstable at Zero List: Very likely to Loll and settle on one of the outriggers Neutrally Stable: until deck hits water Very tender roll characteristic