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A Method of Rapidly Estimating Propeller Moment

Published online by Cambridge University Press:  28 July 2016

P. R. Payne*
Affiliation:
Auster Aircraft Ltd.

Extract

In a Technical Note published in the April 1954 issue of the JOURNAL an approximate equation was presented for calculating the propeller moment of a helicopter rotor at the project stage, the solution to which could be obtained from two graphs.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1954

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