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ITTC – Recommen<strong>de</strong>d<br />

Procedures<br />

Performance, Propulsion<br />

1978 ITTC Performance Prediction<br />

Method<br />

7.5 – 02<br />

03 – 01.4<br />

Page 6 of 31<br />

Effective Date<br />

1999<br />

Revision<br />

00<br />

for the <strong>de</strong>livered power.<br />

Trial prediction with ∆C FC - ∆w C corrections<br />

If CHOICE=1 the final trial predictions are<br />

calculated as follows:<br />

K<br />

J<br />

=<br />

S<br />

.<br />

C<br />

T<br />

TS<br />

2 2D<br />

2<br />

1<br />

+ ∆C<br />

( 1 − t)( − w + ∆w<br />

) 2<br />

With this K T /J² as input value, J TS and K QTS<br />

are read off from the full scale propeller characteristics<br />

and<br />

n<br />

P<br />

T<br />

DT<br />

( 1 − w + ∆w<br />

)<br />

TS<br />

FC<br />

TS C<br />

VS<br />

= (r/s)<br />

J . D<br />

= 2<br />

TS<br />

K<br />

5 3 QTS −3<br />

π . ρ.<br />

D . nT<br />

. .10 (kW)<br />

η<br />

RM<br />

Trial prediction with C NP correction<br />

If CHOICE = 2 the shaft rate of rotation is predicted<br />

on the basis of power i<strong>de</strong>ntity as follows.<br />

⎛ KQ<br />

⎞<br />

⎜<br />

J ³<br />

⎟<br />

⎝ ⎠<br />

T<br />

1000. C<br />

P<br />

. PDS<br />

=<br />

3<br />

2π<br />

. ρ.<br />

D²<br />

V ( 1 − w )³<br />

S<br />

TS<br />

C<br />

2.5 Analysis of Speed Trial Results<br />

The analysis of trials data is performed in a<br />

way consistent with performance prediction but<br />

starting P D and n backwards, i.e. from<br />

K<br />

Q<br />

PD<br />

=<br />

2π<br />

. ρ.<br />

D<br />

. n<br />

. η<br />

5 3 RM<br />

.10³<br />

J S is obtained from the full-scale open-water<br />

characteristics K Q ≈ J S then<br />

w<br />

= 1 − J<br />

. n.<br />

D<br />

T S<br />

/<br />

Further from K T ≈ J S characteristics<br />

T = K<br />

T<br />

. ρ.<br />

n²<br />

D<br />

( 1 − t)<br />

T.<br />

C T<br />

=<br />

1<br />

. ρ.<br />

V ². S<br />

2<br />

Then we obtain<br />

∆ C = C − C<br />

∆ w<br />

FC<br />

C<br />

= w<br />

2.6 Input Data<br />

T<br />

TS<br />

4<br />

− w<br />

Input data sheets are given in ENCL.1<br />

TS<br />

T<br />

V<br />

K<br />

Q0<br />

J ³<br />

⎛ K<br />

=<br />

⎜<br />

⎝ J<br />

Q<br />

⎞<br />

⎟<br />

⎠<br />

T<br />

.η<br />

RM<br />

( 1 − w )/<br />

J D<br />

nS = VS<br />

TS TS<br />

.<br />

n = C<br />

T<br />

NP<br />

n<br />

S<br />

2.7 Output Data<br />

- Output data I gives ITTC Standard Prediction<br />

with C P = C N = 1.0, together with<br />

mo<strong>de</strong>l and full scale propulsive coefficients<br />

(ENCL. 4).<br />

- Output data II gives the final ship prediction<br />

(ENCL. 5).

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