Technical Paper
One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor
1987-10-01
871851
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.
