The results of a study to design a High-Speed Civilian Transport (HSCT) using the blended wing-body configuration are presented. The HSCT is a Mach 2 to 5 transport aircraft designed to compete with current commercial aircraft. The subjects discussed are sizing, configuration, aerodynamics, stability and control, propulsion, performance, structures and pollution effects.
The Horizon: A blended wing aircraft configuration design project, volume 3
1988-06-11
Report
No indication
English
Aerodynamic Analysis of a Blended Wing Aircraft Configuration
British Library Conference Proceedings | 2005
|AERODYNAMIC PERFORMANCE OF A BLENDED-WING-BODY CONFIGURATION AIRCRAFT
British Library Conference Proceedings | 2006
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