Author: Gerald V. FosterPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30
Book Description
Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01
Author: Gerald V. FosterPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30
Book Description
Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01
Author: Static 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
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: Static 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: Static Aerodynamic Characteristics of Several Hypersonic Missile-and-control Configurations at a Mach Number of 4.65
Author: J. D. ChurchSupersonic Aerodynamic Characteristics of a Cruciform Missile Configuration with Low-a-spect-ratio Wings and In-line Tail Controls
Author: Effect of Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers
Author: A. B. Jr BlairEffect on Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers
Author: A. B. BlairPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Book Description
Author: Ross B. Robinson