WIND TUNNEL TEST RESULTS FOR A CANARD ROTOR/WING AIRCRAFT CONFIGURATION
Annual forum; 57th, American Helicopter Society ; 2001 ; Washington, DC
2001-01-01
13 pages
Also known as FORUM 57
Aufsatz (Konferenz)
Englisch
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Low-Speed Wind-Tunnel Test Results of the Canard Rotor/Wing Concept
British Library Conference Proceedings | 1993
|Canard rotor - wing demonstrator
Online Contents | 1993