Author: George C. Jr AshbyPublisher:
ISBN:
Category :
Languages : en
Pages : 124
Book Description
Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and a Number of Trailing Edge and Fin Tip Controls at Mach Numbers from 2.21 to 6.01
Author: George C. Jr AshbyLongitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and Number of Trailing Edge and Fin Tip Controls at Mach Nubmers from 2.21 to 6.01
Author: Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont
Author: Longitudinal Stability and Control Characteristics of a Generalized Missile Configuration Employing Several Different Bulk Type Control Schemes at a Mach Number of 6.01
Author: Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing Edge Flaps and One Having a Flared Afterbody and All Movable Controls
Author: Leroy M. SpearmanStatic Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces
Author: Ross B. RobinsonPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32
Book Description
Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87
Author: Donald T. GregoryPublisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Author: 
Author: Ross B. Robinson
Author: