Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration

Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration
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Total Pages: 124
Release: 1962
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Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20
Language: en
Pages: 54
Authors: Gerald V. Foster
Categories: Airplanes, Tailless
Type: BOOK - Published: 1964 - Publisher:

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Aerodynamic Characteristics at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Language: en
Pages: 53
Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6
Language: en
Pages: 108
Authors: Walter P. Nelms
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1971 - Publisher:

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Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The confi
Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
Language: en
Pages: 68
Authors: A. Warner Robins
Categories: Hypersonic planes
Type: BOOK - Published: 1979 - Publisher:

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