Rotor load requirements as to speed control, torque demands, altitude and temperature performance, transient loads, etc; types of engines and their possibilities of accurate load matching; basic experiences obtained by Kaman Aircraft Corp in powering helicopter with direct driving shaft turbine of Boeing 502 freewheel type; illustrations. Before Am Soc Mech Engrs.
Theory and practice of gas turbine power plants for helicopters
Am Helicopter
American Helicopter ; 30 , n 6-7
1953
7 pages
Aufsatz (Zeitschrift)
Englisch
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