Transonic Wind-Tunnel Investigation of the Effect of Control Span and Large Wing-Tip Nacelles on Effectiveness of Spoiler-Slot- Deflector Controls on an Unswept-Wing Fighter-Type Airplane
1960
34 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft control , Control surface , Nacelle , Wind tunnel , Aircraft , Control , Deflector , Effectiveness , Slot , Span , Spoiler , Stability , Surface , System , Tip , Transonic , Tunnel , Wind , Wing