Test covered transition speed range from hovering to normal flight with flaps retracted; variables in testing were flap deflection, thrust coefficient, stabilizer incidence, ground proximity, and blowing boundary layer control effectiveness.
Investigation of longitudinal and lateral stability characteristics of six-propeller deflected-slipstream VTOL model with boundary-layer control including effects of ground proximity
NASA -- Tech Note
1960
98 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.