Investigation of Control Effectiveness and Stability Characteristics of a Model of a Low-Wing Missile with Interdigitated Tail Surfaces at Mach Numbers of 2.29, 2.97, AND 3.51
1958
33 pages
Report
No indication
English
Aerodynamics , Control stability , Missile , Stability and control , Wind tunnel stability test , Control , Longitudinal , Low wing , Mach number , Model , Speed , Stability , Supersonic , Test , Tunnel , Wind