Design changes that lead to improved aerodynamic and structural efficiency are presented. Practical design constraints and approaches for a blended wing-fuselage are discussed, as well as the integration of the configuration that leads to aerodynamic and structural efficiency. Highlighted are new approaches used to provide for structural efficiency, airline/passenger acceptance, passenger evacuation, and subsystem integration. Results of full-scale passenger cabin mock-up evaluations are presented showing the feasibility of the concept.
Toward a second generation fuel efficient supersonic cruise aircraft
01.01.1976
Aufsatz (Konferenz)
Keine Angabe
Englisch
III. Supersonic Cruise Aircraft
NTRS | 1960
|Advanced supersonic cruise aircraft technology
NTRS | 1977
|Fabrication research for supersonic cruise aircraft
Tema Archiv | 1979
|