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Impact of Bypass Ratio on Thrust-to-Weight for V/STOL
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English
Abstract
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.
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Citation
Wilson, S. and Mahoney, K., "Impact of Bypass Ratio on Thrust-to-Weight for V/STOL," SAE Technical Paper 872348, 1987, https://doi.org/10.4271/872348.Also In
References
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