Study of several primary light weight torque and jet reaction systems which have been contemplated for propulsion power; systems compared with conventional engine now in use; comparison made on basis of hovering endurance and maximum range at forward speed of 75 mph for helicopters having same gross weight.
Analysis of helicopter propulsion systems
Am Soc Mech Engrs -- Trans
1951
9 pages
Aufsatz (Zeitschrift)
Englisch
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