Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing PDF Download
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Languages : en
Pages : 54
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Category :
Languages : en
Pages : 54
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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.
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Languages : en
Pages : 44
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Category :
Languages : en
Pages : 34
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Category : Aeronautics
Languages : en
Pages : 836
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Author: Charles Trescot (D. Jr)
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Category :
Languages : en
Pages : 52
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 2084
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 2300
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Category : Aeronautics
Languages : en
Pages : 704
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Category : Government publications
Languages : en
Pages : 1990
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