NOTA Large Angle Stability 2009
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Transcript of NOTA Large Angle Stability 2009
© Omar Yaakob 2009 1
© Omar Yaakob 2009 87
WB 1
K
Z
M
G
B
W 1
W
ExternalHeelingmoment
M
G Z
L
L1
righting moment = x GZ
for small angles,
GZ = GMT
sin
where is the angle of heel.
Righting Lever and Moment
16. LARGE ANGLE STABILITY
© Omar Yaakob 2009 88
T
TIBM
M’TM
GZ at Large Angles
The location of the metacentre is no longerstationary at large angles. This is due to thedifferent shapes of waterplane areas atsuccessive angle of heels. This differencesgive rise to different transverse secondmoments of area. The distance from thecentre of buoyancy to the metacentre isgiven as
At small angle of heel, IT can be assumedconstant and hence the metacentre can beconsidered stationary. However at largerangles of heels, the waterplane shapeschanges significantly leading to movementof the metacentre . Because of this reason,the accuracy of the expression GZ=GMT sindiminishes at large angles. In other wordsthere is no simple expression relating GZ toGMT .
B’’
B ’
G
© Omar Yaakob 2009 89
GZ or Statical Stability or RightingArm CurvesShows relationship between GZand .
20
GZ
(m)
GZ value at 20
Angle of heel
Angle of Vanishing Stability
Range of Stability
Point of inflexion
At the design stage, the naval architectmust ensure that the curves arecalculated.The GZ data is produced at differentdisplacements. An assumed KG is used.Later, when the actual and KG at anyloading condition are known, actual valuesof GZ can be extracted from the data.
Various methods are used to calculatestatical stability curves. We do not havethe opportunity to deal with these methodsin this short course. Details can be foundin Principles of Naval Architecture (Vol 1).
© Omar Yaakob 2009 90
2,000
5
80
15
50
30
40SN (m)
KS= 4.2m
Cross Curves of StabilityThe GZ values calculated at the designstage are presented either in tables or in
Cross Curves of Stability.The GZ values calculated are carried out atonly a few displacements and heel angles.To obtain values at other displacements or
angles, linear interpolation is used.The values of GZ will depend on the KG butthe value of KG changes from time to time.Since it is difficult to calculate GZ at manydisplacements, various angles of heel anddifferent values of KG, a fixed value of KG
is normally used in the design stage.This assumed position of G is designated S,
the height above keel being KS, thecorresponding point on the line of action ofbuoyancy is called N i.e. not Z. The valueof the righting lever is thus SN instead of
GZ.
2,500
Displacement ( tonnes)
1,500 3,000
© Omar Yaakob 2009 91
N
K
M
G
B
Z
S
N
If S is above G ; GZ = SN + SG SinIf S is below G; GZ = SN - SG Sin
A better method is to put S at the keel i.e.KS=0. In this case SN = KN. The assumedrighting arm, KN values are plotted instead of
SN at various displacement. When G isknown for any condition, GZ can be
calculated:GZ = KN – KG Sin
It must be noted that the values of KG usedis the virtual or fluid KG i.e. taking into
consideration the FSC.
© Omar Yaakob 2009 92
ExampleA ship with lightship displacement 1,700 tonnes, KG 3.5m is load ed with 1,800tonnes of cargo at Kg 3.8m. KMT after loading is 3.8m while KN values are asfollows. Plot the GZ curve and find the area under the curve up to 300.
3.263.252.922.201.540.774,000
3.263.192.842.161.500.753,000
756045302010Displacement(tonnes)
Angle of heel ()
Solution:i. Carry out loading calculation to obtain final displacement and KG.ii. Find KN values at that displacement.iii. Correct KN to obtain GZ using GZ = KN – KG siniv. Plot the curve (note that initial slope= GMT=0.15m)v. Use Simpson rule to find area under the curve up to 30 .
© Omar Yaakob 2009 2
© Omar Yaakob 2009 93
(ii) (iii) (v)
-0.2663.5260.9663.2675
0.0593.1610.8663.2260
1.549sum0.2992.5810.7072.8845
0.35510.3551.8250.5002.1830
0.81530.2721.2480.3421.5220
0.37930.1260.6340.1740.7610
0100000
fASMGZ(m)KG Sin Sin KN(m)
Area under the curve up to 30 ,
Area = 3 x 10 xx 1.549 = 0.1014 mrad8 180
© Omar Yaakob 2009 94
Loading Calculation Table
Initial Ship ConditionΔ, KG, LCG
SHIP HULL FORM
New deadweightloading/unloadingw, Kg, lcg
Calculate DraughtsTA and TF
Use Δto read
Hydrostatics dataTmean, LCB, LCF,MCTC,
KMT
FINALΔ,KG, FSC LCG
Calculate GMT
HydrostaticsData
LOADINGCALCULATIONS
© Omar Yaakob 2009 95
Loading Calculation Table
Initial Ship ConditionΔ, KG, LCG
SHIP HULL FORM
New deadweightloading/unloadingw, Kg, lcg
Calculate DraughtsTA and TF
Use Δto read
Hydrostatics dataTmean, LCB, LCF,MCTC,
KMT
FINALΔ,KG, FSC LCG
Calculate GMT
HydrostaticsData
SN or KN CrossCurvesStability
GZ CURVE
StabilityAssessment
KN/SN Valuesat correctΔ
STABILITYASSESSMENT PROCESS
© Omar Yaakob 2009 96
© Omar Yaakob 2009 97
© Omar Yaakob 2009 98Title: Small Ship Survey- Stability Dr. Omar Yaakob
© Omar Yaakob 2009 3
© Omar Yaakob 2009 99Title: Small Ship Survey- Stability Dr. Omar Yaakob
© Omar Yaakob 2009 100
Large Ship(IMO)Stability Criteria
0.15 mInitial GM6.
25.0 degAngle at Maximum GZ5.
0.20 mMaximum GZ4.
0.03 m radArea Under Curve 30o-40o
or up to f (flooding Angle)3.
0.090 mrad
Area Under Curve 0 o-40o orup to f (flooding Angle)
2.
0.055m.rad
Area Under Curve 0 o-30o1.
© Omar Yaakob 2009 101
7.6.1 Load Line Criteria.
0.35 m0.15 m8. Initial GM
30 deg15 deg7. Angle at Maximum GZ
0.2 m0.2 m6. Maximum GZ
0.03 m.rad0.03 m.rad5. Area Under Curve 30o-40o orup to qf (flooding Angle)
N.A0.055 + 0.001(30-qmax) if max.GZ occur between 15 to 30 deg.4. Area Under Curve 15o-30o
0.089 m.radN.A3 Area Under Curve 0o-40o orup to qf (flooding Angle)
0.055 m.rad0.055 m.rad if max. GZ occur at30 deg.
2. Area Under Curve 0o-30o
N.A0.07 m.rad if max. GZ occur at15 to 30 deg.1. Area Under Curve 0o-15o
Fishing Vessel(IMO)
Small Craft -Passenger/Cargo(HSC Code)Stability Criteria
© Omar Yaakob 2009 102
The stability is assessed at a number of loading conditions depe ndingon ship types, for example:
1. Lightship2. Homogenous Full Load Departure3. Homogenous Full Load Arrival4. Ballast Departure5. Ballast Arrival6. Etc.
© Omar Yaakob 2009 103
ExampleA ship 144m LBP lightship 5200 tonnes, KG 7.4m, LCG 2.0m aft of amidships. Thehomogenous loaded departure condition are as follows:
----
44.0 F17.0 F22.0 A49.0 F
10.17.18.09.0
1700190018001330
Cargo No.1Cargo No.2Cargo No.3Cargo No.4
-14.0 F9.550Crew and Store
21060.0 F7.2170Fresh Water
270350
1.2 A8.0 A
1.53.2
1350210
Fuel Tank 1Fuel Tank 2
FSM(tm)
LCG fromamidship(m)
VCG(m)
Mass(t)
Item
© Omar Yaakob 2009 104
Extracts of hydrostatics data at two relevant draughts are as follows:
8.0837.0883.00178.5613,9999.00
7.956.802.80170.012,9948.50
KMT
(m)LCF(m from)
LCB(m from)
MCTC(tm )
Displacement(tonnes)
T (m)
KN values at two displacements are as follows:
7.0716.5775.5594.0542.1241.4140.70713900
7.0676.5755.5554.0522.1221.4120.70513500
7560453015105o
Find the draughts at the perpendiculars, calculate GMT and check if the vessel pass theIMO merchant ship stability criteria.
© Omar Yaakob 2009 4
© Omar Yaakob 2009 105
1078001286709990613710FINALDISPLACEMENT
830107800118270614268510DEADWEIGHT
---
7480032300
-
--
3960065170
44.0 F17.0 F22.0 A49.0 F
17170134901440011970
10.17.18.09.0
1700190018001330
Cargo No.1Cargo No.2Cargo No.3Cargo No.4
-1020014.0 F4759.550Crew and Store
210-1020060.0 F12247.2170Fresh Water
270350
--
16201680
1.2 A8.0 A
2025675
1.53.2
1350210
Fuel Tank 1Fuel Tank 2
--104002.0 A384807.45200LIGHTSHIP
FSM(tm)
M F(tm)
MA(tm)
LCG from(m from )
M v(tm)
VCG(m)
Mass(t)
Item
KG = 7.287m LCG = 1.52m aft of amidships Free Surface Correction, F.S.C = 0.061m
© Omar Yaakob 2009 106
GMSOLID
= mF.S.C = m
GMFluid
= m
Title: SHIP STABILITY – Dr. Omar Bin Yaakob
1299413999
1299413710
Enter hydrostatic Table at = 13710 tonnes, to obtain:
Tmean
= 8.50 + (9.00 – 8.50)
= 8.856m
and,MCTC = 176.1 t.m. ; KM
T= 8.045 m;
LCB = 2.949 m.A.LCF = 7.005 m.A.
For transverse stabilityKM = mKG = m
© Omar Yaakob 2009 107
TRIM = by bow/stern
100)(
MCTCxxp
TA = T mean ± TA
TF = T mean ± TF
For longitudinal stability
TRIM =
TA= trim x (72 – )144
= m
TF=
© Omar Yaakob 2009 108
GZ (m)
KGf sin
7.0696.5765.5574.0532.1231.4130.706KN (m)
7560453015105o
KGf = 7.287 + 0.061GZ = KN - KGf Sin Plot GZ curve and calculate and check criteria.
OK>0.15m0.697mGMT
OK0.03 m-rad0.072 m.radA40
– A30
OK0.09 m-rad0.187 m.radA40
OK0.055 m-rad0.115 m.radA30
OK0.2m @ 30 0.393m @ 37GZmax
EvaluationRequired by IMORule
ActualCriteria
i.e. fulfill all Load Line Rule Criteria
Values obtainedfrom KN Table atDisplacement =13,710 tonnes
KG fluid, takinginto account freesurfacecorrection
© Omar Yaakob 2009 109
Determining Steady Angle of Heel due to Heeling Moment
Righting moment = Righting Lever x = GZ
Curves of displacement multiplied by GZ values at various angles of heel are called therighting moment curve.
When a ship is acted upon by an external or internal moments, the steady angle of heel canbe obtained as the point of equilibrium between the curves of heeling moment and the rightingmoment curve.
Heeling mmnt cos
Steady Angle of Heel
Moment
Heel angle
GZ
A
D
cDE
E
F
© Omar Yaakob 2009 110
The same information can be represented using the righting arm (instead of rightingmoment) curve and curveHeeling moment cos
Heeling mmt cos
Steady Angle of Heel Heel angle
GZ
AD
cDE
E
F
Arm (m)We are not only concerned aboutthe resultant steady angle of heelbut also possibility ofovershooting.
US Navy Criteria:•For crowding of personnel and lifting of weight:•Angle at C for lifting of weight or crowding of personnel < 15 degrees•Heeling arm at C < 0.6 maximum•Area A1 > 0.4 total area under curve.
Area 1
© Omar Yaakob 2009 5
© Omar Yaakob 2009 111
During operation, the craft has always been expected toencounter the heeling arm or upsetting arm due to :
• wind,• lifting of weight,• movement of personnel and• high speed turning.
The effect of heeling arm need to be calculated and assessedagainst the specified criteria.
Presently, the stability of ship subjected to heeling arm isassessed statically that is by superimposing the heelingarm curve onto the GZ curve.
Effect of Heeling Arm
© Omar Yaakob 2009 112Title: Small Ship Survey- Stability Dr. Omar Yaakob
Heeling Arm Curve Due to Turning at High Speed,Movement of Personnel and Lifting of Cargo
© Omar Yaakob 2009 113Title: Small Ship Survey- Stability Dr. Omar Yaakob
Heeling Arm Curve Due to Wind and Wave
© Omar Yaakob 2009 114Title: Small Ship Survey- Stability Dr. Omar Yaakob
Stability Criteria For Small Craft Under Heeling Arm
A1 > 0.4 Area UnderGZ Curve
A1 > 0.4 Area UnderGZ Curve
6. Area Under Curve For HighSpeedTurning
A1 > 1.4 A2A1 > 1.4 A25. Area Under Curve For BeamWind
0.6 of GZ max0.6 of GZ max4. GZ at Intersection Point (c)
15deg10 deg
3 Max Angle of Heel atIntersectionPoint (c) For Movement ofPersonnel
15deg8 deg
2. Max Angle of Heel atIntersectionPoint (c) For High SpeedTurning
15deg10 deg
1. Max Angle of Heel atIntersectionPoint (c) For Beam Wind
Fishing Vessel(IMO)
Small Craft -Passenger/Cargo(IMO and HSCCode)
Stability Criteria
© Omar Yaakob 2009 115
EXERCISES
1. For one loading condition, a ship LBP 70m has displacement 1500 tonnes, KG 4.0 mand KM 4.5 m. SN values calculated at KS=4.2m are given in the table below.
0.010.190.350.440.440.350.23SN (m)
75604530201510Angle()
a.Plot the GZ curve of the vessel.b.Check if the ship passes Load Line Rule stability criteria.c.Find the angle of heel if a 50 tonne weight already onboard is moved 10 m across.
© Omar Yaakob 2009 116
GZ (m)
SG sin
SN (m)
7560453015105o
pass>0.15m0.5mGMT
pass0.03 m-rad0.09A40 – A30
pass0.09 m-rad0.28A40
pass0.055 m-rad0.188A30
pass0.2m @ 25 0.54m at 30 degGZmax
EvaluationRequiredActualCriteria
i.e. fulfill all Load Line Rule Criteria
Since KS > KG, S is above G ; so GZ = SN + SG Sin
© Omar Yaakob 2009 6
© Omar Yaakob 2009 117
2. A fishing boat began its trip with displacement of 340 tonnes , KG 3.5 m and KM 3.75m. After one day journey, the following events occurred :
20 tonne fish loaded (kg 3.0m)6 tonne fuel consumed (kg 1.0m)4 tonne fresh water consumed (kg 2.0m)
KM was found to be 3.8 m. The KN values are as follows:
a. Plot its GZ Curveb. In this condition the boat then used the power block to lower a small boat to sea.
The weight of smal boat was 10 tonne and the boom of the power block was 4from the boat’s centreline on the starboard side and 5 m above keel. Plotroughly (but do not calculate) the new righting arm curve and estimate itssteady angle of heel.
3.453.292.992.281.5210.710400
3.553.373.072.401.5250.720300
906045302010Displacement(tonne)
Angle of Heel
© Omar Yaakob 2009 118
GZ (m)
KGf
sin
KN (m)
o
KG= 3.53mGZ = KN - KG Sin .
Item Weight(tonnes)
KG (m) Moment about keel (tonne-m)
TOTAL
© Omar Yaakob 2009 119
3. A ship 150m LBP has lightship displacement 6500 tonnes, KG 8.0 m, LCG 1.5 m aftof amidships. The ship is loaded as follows :
44.0 F17.0 F22.0 A
10.17.18.0
180020001600
Cargo Hold No.1Cargo Hold No.2Cargo Hold No.3
14.0 F9.550Crew and Store
60.0 F7.2200Fresh water Tank
1.2 A8.0 A
1.53.2
1000300
Fuel Tank 1Fuel Tank 2
LCG from amidships(m)
VCG(m)
Mass(t)
Item
* free surface effect is neglectedExtract of hydrostatics data at relevant draughts as follows:
8.082.30A3.01F180.513,50010.00
7.951.80A2.85F176.613,4009.50
KMT (m)LCF(m dari)
LCB(m dari)
MCTC (tm )Displacement (tonnes)T (m)
© Omar Yaakob 2009 120
7.0696.5765.5574.0532.1231.4130.70613,500
6.8736.3465.2684.0002.0231.4000.70013,400
7560453015105
o
(tonnes)
KN values in meters at two displacements are as follows:
a. Find Draughts at the perpendicularsb. Find GM T.c. Calculate and plot the righting arm curve of the ship. Check whe ther
the vessel passes stability criteria for merchant ship.d. Estimate its angle of heel when the ship is lifting a 200 tonne cargo
on the port side using its own derrick. The derrick head is 15 m fromthe centreline and 15 m above keel.
e. It is desired to reduce this heel angle to 5 degrees. How muchballast water must be transferred from port tank to starboard ta nk, adistance 6 meters?