Hypersonic Aerodynamic Characteristics of a Lifting Reentry Vehicle Model with Four Types of Longitudinal Control Surfaces PDF Download
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Author: Charles Trescot (D. Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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Book Description
Author: Charles Trescot (D. Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 62
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Author: William O. Armstrong
Publisher:
ISBN:
Category :
Languages : en
Pages : 102
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Author: Ernst Heinrich Hirschel
Publisher: Springer Science & Business Media
ISBN: 354089974X
Category : Technology & Engineering
Languages : en
Pages : 512
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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.
Author: Robert Charles Goetz
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 60
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Author: Charles H. Fox
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Mukkarum Husain
Publisher: LAP Lambert Academic Publishing
ISBN: 9783845406374
Category :
Languages : en
Pages : 100
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Book Description
Maneuverability of re-entry vehicles can be improved notably simply by modifying the geometric characteristics of the vehicles. The objective of the present work is to study the aerodynamic characteristics of different asymmetric re-entry vehicles. An algorithm based on Yee, Sandham, and Djomehri's high resolution, low dissipation numerical scheme is constructed, and the associated computational code is developed. This developed code is then validated by different test cases. Aerodynamic performances of asymmetric re-entry vehicles with different configurations and orientations are computed using the low dissipative high resolution artificial compression method. Upper portion of a symmetrical blunt body is cut by three different plane surfaces at three different locations to generate asymmetric blunt bodies. Effects of cutting plane angles and locations are studied. Present study shows that, for a given range of angles of attack and flight conditions, improved lift and stability in longitudinal plane and better control in transverse plane can be achieved by generating appropriate asymmetric re-entry vehicles.
Author: Frances E. Sabo
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 182
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Book Description
