Development of current propeller theory and practice to cover range of aircraft speeds between 450 and 550 mph, which, at 36,000 ft represents flight Mach number range of 0.68 to 0.83; comparative efficiencies of propeller turbine and turbojet systems; propeller noise; propeller solidity; blade section characteristics; flutter; blade root sections and spinners; structural strength; future trends.
Propellers for high-speed aircraft
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 58 , n 528
1954
9 pages
Aufsatz (Zeitschrift)
Englisch
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PROPELLERS FOR HIGH SPEED AIRCRAFT
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