One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor 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.
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. Download Citation
Author(s):
James R. Arnold, Michelle Corning, Michael K. Farrell
Affiliated:
Federal Aviation Administration
Pages: 10
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
Type Certification of New Aircraft Technology-SP-0727, SAE 1987 Transactions: Aerospace-V96-6
Related Topics:
Aircraft
Entry, descent, and landing
Propellers and rotors
Certification
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