Fixed-wing performance predictions of the Canard rotor/wing concept based on wind tunnel test results
13th Applied Aerodynamics Conference ; 1995 ; San Diego , CA , U.S.A.
01.01.1995
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Low-Speed Wind-Tunnel Test Results of the Canard Rotor/Wing Concept
British Library Conference Proceedings | 1993
|WIND TUNNEL TEST RESULTS FOR A CANARD ROTOR/WING AIRCRAFT CONFIGURATION
British Library Conference Proceedings | 2001
|Canard Rotor/Wing UAV Platform Concept
British Library Conference Proceedings | 1993
|