Aerodynamic Characteristics at Low Speed of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Language: en
Pages: 44
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
NASA Technical Note
Language: en
Pages: 842
Authors:
Categories:
Type: BOOK - Published: 1963 - Publisher:

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Low-speed Longitudinal Stability Characteristics of a Supersonic Transport Configuration with Variable-sweep Wings Employing a Double Inboard Pivot
Language: en
Pages: 56