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One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor
ISSN: 0148-7191, e-ISSN: 2688-3627
Published October 01, 1987 by SAE International in United States
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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.
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