Manoeuvring Flashcards

1
Q

What are Yv’, Nv’, Yr’, and Nr’?

A
' non dimensional
Y is sway force
N is yaw moment
r is yaw rate
v is sway velocity
So Yr' is the non dimensional rate of change of sway force wrt yaw rate
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2
Q

Give the equation for stability

A

(Nr’-m’Xg’)/(Yr’-m’)>Nv’/Yv’

N on top y on bottom

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3
Q

If the stability equation gives an unstable condition, give the new stability equation (with an autopilot)

A

(Nr’-m’Xg’+bNδ’)/(Yr’-m’+bYδ’)>Nv’/Yv’

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4
Q

Why is manoeuvring important?

A

For the protection of persons, property, and the environment. From contacts, groundings, collisions.

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5
Q

What are the six degrees of freedom and give their numbers? Which three are used in manoeuvring?

A

1) surge. 2) sway. 3) heave. 4) roll. 5) pitch 6) yaw. Surge sway and yaw are used in manoeuvring

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6
Q

Name the different types of rudders.

A

Balanced, spade, full skeg, semi balanced skeg,

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7
Q

What 3 things are carried on ships for manoeuvring criteria?

A

Pilot card, wheel house poster and manoeuvring booklet

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8
Q

Give the different types of manoeuvring trials.

A

Turning ability test, initial turning test, course keeping ability (zigzag), stopping tests, pull out test and spiral test. The last two are only for when dynamic instability is indicated in the results of the standard tests

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9
Q

How do you find the rate of change of sway force wrt sway velocity and the rate of change of yaw moment wrt sway velocity?

A

Static drift test. Measure Y and N for given β. β is proportional to sway velocity so can plot Y and N against sway velocity get straight line graphs with negative gradient. Angle is dY/dv and dN/dv

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10
Q

Describe a static drift test.

A

In a towing tank. Set model at a drift angle β and measure the resulting sway force and yaw moment. For a given carriage speed sway velocity is directly proportional to drift angle. Repeat for various drift angles. Plot a graph of Y against v and N against v

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11
Q

How do you find the rate of change of sway force (and yaw moment) wrt yaw rate?

A

Rotating arm test. For a range of arm radii (from which carriage rate and yaw rate can be found) measure sway force and yaw moment. Plot these against yaw rate. Get graphs with negative gradient straight line. The angle is dY/dr and dN/dr.

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12
Q

Describe a rotating arm test.

A

Set the rotating arm radius and measure the forces and moments. Yaw rate is proportional to radius for a given carriage rate. Test for a range of arm radii so that a plot of yaw moment and sway force against yaw rate can be plotted.

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13
Q

How do you fined the rat of change of yaw moment (and sway force) wrt rudder angle?

A

Using rudder tests where there is no sway velocity but various rudder angles the yaw moment and sway forces can be measured. These are plotted on graphs where the gradient is dY/dδ and dN/dΔ

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14
Q

What are hydrodynamic forces predominantly dependent upon?

A

Density, velocity, gravity, length, viscosity (m2/s)

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15
Q

How do you non dimensionalise a force (what do you divide by)? And therefore how do you non dimensionalise a moment?

A

Divide by 0.5ρv^2L^2

For a moment divide by 0.5ρv^2L^3

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16
Q

How do you check for dynamic stability in the characteristic equation? What must T1’ and T2’ be?

A

All the roots should have negative real parts therefore T1’ and T2’ should be positive

17
Q

What does thestability equation tell us?

A

That the centre of pressure in pure yaw must be ahead of the centre of pressure in pure sway if the ship is to possess positive directional stability

18
Q

Give the equation for a simple autopilot.

A

δ=br’

19
Q

Giv wthe conditions of constants for an autopilot for stability.

A

C-Eb>0

20
Q

What is K’ and how do you calculate it?

A

The non dimensionalise gain constant.

K’=-((ψ1-ψ2)/(integral(δdt’)))
Integral between t1’ and t2’

21
Q

What is T’ and how do you calculate it?

A

Non dimensional time constant.

K’/T’=-(r3’-r4’)/integralδdt’

Integrate between t3’ and t4’