Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2

Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2
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ISBN-10 : OCLC:842468263
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Book Synopsis Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 by : William B. Igoe

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Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 Related Books

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
Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number of the Square Root of 2
Language: en
Pages: 1
Authors: MARLOWE D. CASSETTI
Categories:
Type: BOOK - Published: 1961 - Publisher:

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A inves iga io as been made of the effects of conical wing camber and body indentation ccordi g to t e supersonic area rule on the aerodynamic wing loading char
Transonic Aerodynamic Characteristics of a Wingbody Combination Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 1.1416
Language: en
Pages: 1
Authors: WILLIAM B. IGOE
Categories:
Type: BOOK - Published: 1961 - Publisher:

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An investigation was made of the effects of conical wing camber and supersonic body indentation on the aerodynamic characteristics of a wing-body configuration