It is recalled that for a detailed propeller design, theoretical models have to be used which are now available to the designer in computer programs. A brief review of the assumptions, on which various propeller models are based, is given. A procedure in use at the NSMB, for the evaluation of the pressure distribution on the blade sections of a propeller in off-design conditions, is discussed.
Derivation of propeller blade section properties from lifting surface theory1
International Shipbuilding Progress ; 27 , 314 ; 257-267
1980-10-01
11 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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