One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor

871851

10/01/1987

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
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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DOI
https://doi.org/10.4271/871851
Pages
10
Citation
Arnold, J., Corning, M., and Farrell, M., "One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor," SAE Technical Paper 871851, 1987, https://doi.org/10.4271/871851.
Additional Details
Publisher
Published
Oct 1, 1987
Product Code
871851
Content Type
Technical Paper
Language
English