Impact of Bypass Ratio on Thrust-to-Weight for V/STOL
872348
12/01/1987
- Event
- Content
- 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.
- Pages
- 12
- 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.