Author: John P. Jr MuglerPublisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Transonic Wind Tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Five Nose Cones Designed for Supersonic Impact
Author: John P. Jr MuglerA Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0
Author: George C. AshbyPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82
Book Description
Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution
Author: NASA Technical Note
Author: Transonic Dynamic Longitudinal Stability Characteristics of Six Ballistic Reentry Configurations Designed for Supersonic Impact
Author: Aerodynamic Characteristics in Pitch of Six Ballistic Reentry Models at a Mach Number of 10.03
Author: Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact
Author: Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05
Author: Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1116
Book Description
Author: