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Impact of Bypass Ratio on Thrust-to-Weight for V/STOL

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Wilson, Samuel, author.
Conference Name:
SAE International Powered Lift Conference and Exposition (1987-12-07 : Santa Clara, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1987
Summary:
This paper addresses the effect of bypass ratio on thrust-to-weight, fuel flow, and hover efficiency. Four selected representative tilt propulsion system aircraft are analyzed. The paper covers a quantative discussion of the issues involved in selecting a V/STOL propulsion system
Notes:
Vendor supplied data
Publisher Number:
872348
Access Restriction:
Restricted for use by site license

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