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Variable Sweep - Application to the Supersonic Transport Airplane Div., The Boeing Company

SAE Technical Papers (1906-current) Available online

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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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