Investigation of the Aerodynamic Characteristics of a Supersonic Horizontal- Attitude VTOL Airplane Model at Mach Numbers of 1.57, 2.14, 2.54, and 2.87
1960
155 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft model , Lateral stability , Longitudinal stability , Static aerodynamic characteristics , Vtol aircraft , Aerodynamic , Aircraft , Attitude , Characteristics , Drag , Dynamic , Fin , Graph , Horizontal , Lateral , Longitudinal , Model , Pressure , Stability , Stagnation , Static , Supersonic , Tail , Tip , Tunnel , Vertical , Vtol , Wind , Wing