Stability and Control Characteristics at Mach Numbers of 1.41 and 2.20 of a Multimission STOL Airplane Configuration with a Variable-Skew Wing
1963
77 pages
Report
Keine Angabe
Englisch
Aircraft , Body-wing combination , Stability and control , Stol aircraft , Supersonic speed , Angle of attack , Characteristics , Combination , Configuration , Control , Duct , Inlet , Mach number , Rotation , Skew , Speed , Stability , Supersonic , Variable , Wing