Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination

Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination
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Total Pages : 126
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ISBN-10 : OCLC:26432693
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Book Synopsis Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination by : John P. Mugler

Download or read book Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination written by John P. Mugler and published by . This book was released on 1958 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination Related Books

Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination
Language: en
Pages: 126
Authors: John P. Mugler
Categories: Transonic planes
Type: BOOK - Published: 1958 - Publisher:

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Pressure Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing
Language: en
Pages: 80
Authors: Earl R. Keener
Categories: Aerodynamic load
Type: BOOK - Published: 1959 - Publisher:

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Professional Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing
Language: en
Pages: 76
Authors: Earl R. Keener
Categories:
Type: BOOK - Published: 1959 - Publisher:

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Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-aspect-ratio Delta Wing in Combination with Basic and Indented Bodies
Language: en
Pages: 79
Authors: John P. Mugler
Categories: Aerodynamic load
Type: BOOK - Published: 1957 - Publisher:

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Pressure distributions on a thin conical cambered low-aspect-ratio delta wing have been obtained in the Langley 8-foot transonic tunnel over a Mach number range
Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2
Language: en
Pages: 104
Authors: Marlowe D. Cassetti
Categories: Transonic wind tunnels
Type: BOOK - Published: 1961 - Publisher:

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An investigation has been made of the effects of conical wing camber and body indentation according to the supersonic area rule on the aerodynamic wing loading