Author: Ross B. Robinson
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One with Low-aspect-ratio Cruciform Fins and Trailing-edge Flaps and One with a Flared Afterbody and All-movable Controls
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
An Experimental and Theoretical Study of the Aerodynamic Characteristics of Some Generic Missile Concepts at Mach Numbers from 2 to 6.8
Static Aerodynamic Characteristics of Several Hypersonic Missile-and-control Configurations at a Mach Number of 4.65
Supersonic Aerodynamic Characteristics of a Cruciform Missile Configuration with Low-a-spect-ratio Wings and In-line Tail Controls
AIAA 82-0250 - AIAA 82-0300
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
Longitudinal Aerodynamic Characterisitcs of Five Hypersonic Missile Configurations at Mach Numbers from 2.01 to 6.01
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. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30
Book Description