Flowfield and Acoustic Measurements from a Model Tiltrotor in Hover
Author:
Affiliation:
1. United Technologies Research Center, East Hartford, Connecticut 06108-1127
2. Cornell University, Ithaca, New York 14853-7501
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2387
Reference43 articles.
1. Civil Applications of High Speed Rotorcraft and Powered Lift Aircraft Configurations
2. Noise considerations for tiltrotor
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