Effect of Several Tail Configurations on the Stability Characteristics of a Midwing Supersonic-Bomber Model at Mach Numbers of 1.60, 1.90, 2.20, AND 2.50
1960
48 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aerodynamic stability , Aircraft configuration , Aircraft model , Aircraft , Attack , Bomber , Characteristics , Chart , Configuration , Fuselage , Midwing , Model , Stability , Supersonic , Tail , Tunnel , Wind