Preliminary Investigation of Spoiler Lateral Control on a 42 Degree Sweptback Wing at Transonic Speeds PDF Download
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Author: Leslie E. Schneiter
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Author: Leslie E. Schneiter
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Author: United States. Congress. Senate. Committee on the Judiciary
Publisher:
ISBN:
Category : Patent laws and legislation
Languages : en
Pages : 66
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Author: Thomas R. Turner
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ISBN:
Category :
Languages : en
Pages : 35
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 62
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Author: Alexander D. Hammond
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ISBN:
Category : Mach number
Languages : en
Pages : 58
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Author: Alexander D. Hammond
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
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Author: Leslie E. Scneiter
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ISBN:
Category :
Languages : en
Pages : 29
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Author: William C. Sleeman
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ISBN:
Category : Aerofoils
Languages : en
Pages : 34
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This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Author: John G. Lowry
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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