A Summary of the Longitudinal and Lateral Stability and Control Characteristics Obtained from Rocket-Model Tests of a Swept-Wing Fighter-Type Airplane at Mach Numbers from 0.5 to 1.9
1957
86 pages
Report
Keine Angabe
Englisch
Aerodynamics , Fighter aircraft , Lateral stability , Longitudinal control , Stability and control , Swept wing , Aeroelasticity , Aircraft , Coefficient , Control , Drag , Engine , Exhaust , Fighter , Jet , Lateral , Longitudinal , Rolling , Stability , Sweep , Wing