Aerodynamic Characteristics At Mach Numbers From 25 To 35 Of A Canard Bomber Configuration Designed For Supersonic Cruise Flight

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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

Aerodynamic Characteristics at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

Author	: Melvin M. Carmel
Publisher	:
Total Pages	: 53
Release	: 1958
Genre	:
ISBN	:

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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 at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

Authors: Melvin M. Carmel

Categories:

Type: BOOK - Published: 1958 - Publisher:

Aerodynamic Characteristics at Low Speed of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

Language: en
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Aerodynamic Characteristics at Low Speed of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

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Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight

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Pages: 38

Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight

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An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight

Language: en
Pages: 88

An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight

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Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards

Authors: A. Warner Robins

Categories: Hypersonic planes

Type: BOOK - Published: 1979 - Publisher: