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Variable Sweep - Application to the Supersonic Transport Airplane Div., The Boeing Company
- Format:
- Conference/Event
- Author/Creator:
- Swihart, John M., author.
- Conference Name:
- SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1964
- Summary:
- The fundamental aerodynamic benefits of variable sweep are shown to have a strong influence on supersonic transport design. Improved operational characteristics, such as shorter take-off and landings, lower take-off and approach noise, and lower take-off and landing speeds are achieved when compared to the present subsonic jets. A smaller gross weight airplane with smaller engines for a given payload range mission is the result of superior aerodynamic performance when compared to a low aspect ratio fixed geometry approach. The economics of the variable sweep SST are shown to compare favorably with present subsonic jets
- Notes:
- Vendor supplied data
- Publisher Number:
- 640249
- Access Restriction:
- Restricted for use by site license
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