Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2

Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2
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Total Pages : 56
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ISBN-10 : UIUC:30112106590380
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Book Synopsis Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 by : William B. Igoe

Download or read book Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 written by William B. Igoe and published by . This book was released on 1961 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 Related Books

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
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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
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
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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