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Practical Ship Hydrodynamics

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<strong>Ship</strong> manoeuvring 171<br />

it is important to consider that the ship is faster at the beginning of the<br />

turning circle and slower at sustained turning. The heeling angle exceeds<br />

dynamically the statical heel angle due to forces listed above.<br />

The turning circle test is used to evaluate the turning ability of the ship.<br />

2. Spiral manoeuvres<br />

We distinguish between:<br />

– ‘Direct’ spiral manoeuvre (Dieudonne)<br />

With the ship on an initial straight course, the rudder is put hard to one<br />

side until the ship has reached a constant rate of change of heading.<br />

The rudder angle is then decreased in steps (typically 5°, but preferably<br />

less near zero rudder angle) and again held until a steady condition is<br />

reached. This process is repeated until the rudder has covered the whole<br />

range to the maximum rudder angle on the other side. The rate of turn<br />

is noted for each rudder angle. The test should be performed at least for<br />

yaw unstable ships going both from port to starboard and from starboard<br />

to port.<br />

– ‘Indirect’ (reverse) spiral manoeuvre (Bech)<br />

The ship is steered at a constant rate of turn and the mean rudder angle<br />

required to produce this yaw rate is measured. This way, points on the<br />

curve rate of turn vs. rudder angle may be taken in any order.<br />

The spiral test results in a curve as shown in Fig. 5.5. The spiral test is used<br />

to evaluate the turning ability and the yaw stability of the ship. For yaw<br />

unstable ships, there may be three possible rates of turn for one given rudder<br />

angle as shown in Fig. 5.5. The one in the middle (dotted line) represents<br />

an instable state which can only be found by the indirect method. In the<br />

direct method, the rate of turn ‘switches’ at the vertical sections of the<br />

curve suddenly to the other part of the curve if the rudder angle is changed.<br />

This is indicated by the dotted arrows in Fig. 5.5.<br />

Rate of turn Rate of turn<br />

Right (stb)<br />

Curve obtained<br />

from reversed<br />

spiral<br />

Rudder angle d<br />

Rudder angle d<br />

Left (port) Right (stb) Left (port)<br />

Right (stb)<br />

Left (port)<br />

Figure 5.5 Results of spiral tests for yaw stable and yaw unstable ship<br />

Right<br />

Left<br />

(stb)<br />

(port)<br />

Curve obtained<br />

from direct or<br />

reversed spiral<br />

The spiral test, especially with the direct method, is time consuming and<br />

sensitive to external influences. The results show that a linearization of the<br />

body force equations is acceptable only for small jrj (Fig. 5.5). For yaw<br />

stable ships, the bandwidth of acceptable rudder angles to give small jrj is<br />

small, e.g. š5°. For yaw unstable ships, large jrj may result for any υ.

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