Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless delta V/STOL Configuration Having Variable-Sweep Wing Panels
1961
36 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aerodynamic characteristics , Delta wing , Stol aircraft , Tailless aircraft , Variable sweep , Aerodynamic , Aircraft , Characteristic , Control , Delta , Inlet , Mach number , Panel , Planform , Stability , Sweep , Tailless , Twin , Variable , Vertical , Vtol aircraft , Wing