Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg delta Wing
1960
31 pages
Report
No indication
English
Aircraft configuration , Canard , Delta wing , Stability and control , Aerodynamics , Aircraft , Configuration , Control , Delta , High , Low wing , Stability , Supersonic , Test , Trim , Wing