V/STOL wind tunnel data at low forward speeds, discussing test limit dependence on model size, downwash angle and tunnel geometry
Comments on V/STOL wind tunnel data at low forward speeds.
AERODYNAMICS OF ROTARY WING AND V/STOL AIRCRAFT, SYMPOSIUM ; 1969 ; BUFFALO, NY
1969-01-01
Conference paper
No indication
English
Wind-tunnel testing of VTOL and STOL aircraft
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