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Official Records This document is a modern transcription of Admiralty file ADM 226/23, concerning the speed trials of Hood. The original document is held at the The National Archives at Kew, London. This Crown Copyrighted material is reproduced here by kind permission of The National Archives. |
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Haslar 8th June 1921 D.N.C. SPEED TRIALS OF H.M.S. "HOOD". Analysis of Results 1. The Speed Trial records of
the "Hood" forwarded with your reference of the 20th August
1920, have been analysed, and the results are shewn on the accompanying
tracing in the usual "pillar" diagrams i.
These apply to the results for all four shafts collectively. Plottings
are also made for the S.H.P./D.H.P. (see id)
and "x", (i.e. 2. It is a matter for regret that screw experiments for the "Hood" model (YA), were unfortunately only made at high speeds (see Report of 17th Jan 1917), so that the values for the Hull Effy. Elements had to be inferred for the lower speeds. This was done by adopting the same character of curve as was used for the "Renown" and "Repulse" trial analysis, which is fairly well established by a study of the results for similar models (see report of 2nd Feb 1917). The curves adopted are shewn on Sheet I.
4. The drag due to the inner screw running idle at 13.09 and 15.17 knots in the Light Draught Trials is seen from the isolated "pillar" plottings of the H.P. constant at the speeds stated (Sheet II). The extra power needed to overcome the negative thrust of the screws appears to be about 12%, and this (when corrected for the screw efficiency) may presumably be regarded as a measure of the total friction of the propellor, bearings, gear wheels, and "windage" of turbine. The revolutions of the trailing screws were not recorded on the mile, but can be estimated from the appropriate three hours trial, which indicate a negative slip of nearly 18%. It might be expected that these trailing runs would give some idea as to the speeds of the wake stream past the screw disc, but the large negative slip experienced renders any accurate investigation of the wake from such experiments quite out of the question. Exterpolating our propeller data to negative slips (which is of course quite and assumption) it is found that the negative thrust developed by the propeller is in fair accord with the above, and this may be regarded as a rough confirmation of the wake values adopted at these speeds. 5. A striking feature of the
analysis lies in the excess of 6. It is of interest to examine the
possible causes to which this excess of
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