Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62 PDF Download
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Author:
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Category :
Languages : en
Pages : 52
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Author:
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ISBN:
Category :
Languages : en
Pages : 52
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Author: John P. Gapcynski
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Category : Aerodynamic load
Languages : en
Pages : 22
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Author:
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Category :
Languages : en
Pages : 84
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Author:
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Category :
Languages : en
Pages : 86
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Category :
Languages : en
Pages : 46
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Author: Roger H. Fournier
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Category : Space vehicles
Languages : en
Pages : 76
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An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Author: Dennis E. Fuller
Publisher:
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
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Author:
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Category :
Languages : en
Pages : 46
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Author:
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Category :
Languages : en
Pages : 70
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Author:
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ISBN:
Category :
Languages : en
Pages : 44
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