One Engine Inoperative takeoff climb performance of the XV-15 tilt rotor aircraft was analytically determined from level flight data and compared to the proposed powered-lift aircraft criteria. The results of this analysis can be useful in establishing the takeoff profile and highlighting potential certification issues.
One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1987
1987-10-01
Conference paper
English
One engine inoperative takeoff climb performance of the XV-15 tilt rotor
Tema Archive | 1987
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