Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01
1959
24 pages
Report
No indication
English
Missile Technology , Aerodynamics , Fluid Mechanics , Aerodynamic characteristics , Canard , Hypersonic vehicle , Lateral stability and control , Longitudinal stability and control , Pressure tube , Aerodynamic , Afterbody , Angle of attack , Characteristics , Configuration , Control , Cruciform , Fin , Flare , Hypersonic , Lateral , Longitudinal , Moment , Pitch , Pressure , Rolling , Sideslip , Stability , Supersonic , Tube , Tunnel , Vehicle , Wing