Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
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Total Pages : 88
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ISBN-10 : UIUC:30112106666750
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Book Synopsis Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 by : Richard J. Re

Download or read book Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 written by Richard J. Re and published by . This book was released on 1978 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 Related Books

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
Language: en
Pages: 88
Authors: Richard J. Re
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1978 - Publisher:

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Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
Language: en
Pages: 88
Authors: Richard J. Re
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1978 - Publisher:

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Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 to 2.86
Language: en
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Authors: Samuel M. Dollyhigh
Categories: Aerodynamics
Type: BOOK - Published: 1971 - Publisher:

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An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coup
Longitudinal Aerodynamic Characteristic of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
Language: en
Pages: 78
Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 To.2.86
Language: en
Pages: 115
Authors: Samuel M. Dollyhigh
Categories: Aerofoils
Type: BOOK - Published: 1971 - Publisher:

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An experimental investigation has been made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close