Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Aerodynamic Characteristics of Two Winged Reentry Vehicles at Supersonic and Hypersonic Speeds
Author: Aerodynamic Characteristics of a Blunt-nosed Winged Reentry Vehicle at Supersonic and Hypersonic Speeds
Author: Summary of Aerodynamic Characteristics of Low-lift-drag-ratio Reentry Vehicles from Subsonic to Hypersonic Speeds
Author: Hypersonic Aerodynamic Characteristics of a Lifting Reentry Vehicle Model with Four Types of Longitudinal Control Surfaces
Author: Charles Trescot (D. Jr)Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Supersonic and Hypersonic Aerodynamic Characteristics of Two Shuttle-Orbiter Configurations Designed for Reduced Length
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 55
Book Description
Performance, stability, and control tests at supersonic and hypersonic speeds have been performed on two versions of a shuttle orbiter configuration designed for reduced length. One of the test configurations had twin dorsal fins rolled out 15 deg, the other a centerline single dorsal fin. Effects of eleven and body flap deflection, rudder flare, planform fillet, and aileron deflection were examined. The supersonic tests were over the Mach number range from 1.6 to 4.63 at a Reynolds number based on model length of 4.3 x 10(exp 6). The hypersonic tests were conducted at a Mach number of 10.3 and Reynolds number of 0.67 x 10(exp 6). Aerodynamics, Supersonic and hypersonic, Space vehicles.
NASA Technical Note
Author: Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6
Author: Hypersonic Aerodynamic Characteristics of Several Series of Lifting Bodies Applicable to Reentry Vehicle Design
Author: William O. ArmstrongPublisher:
ISBN:
Category :
Languages : en
Pages : 102
Book Description
Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles
Author: Ernst Heinrich HirschelPublisher: Springer Science & Business Media
ISBN: 354089974X
Category : Technology & Engineering
Languages : en
Pages : 512
Book Description
In this book selected aerothermodynamic design problems in hypersonic vehicles are treated. Where applicable, it emphasizes the fact that outer surfaces of hypersonic vehicles primarily are radiation-cooled, an interdisciplinary topic with many implications.
An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack
Author: Robert H. FeldhuhnPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 148
Book Description
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.