Whirl Flutter Investigation of Hingeless Proprotors
Author:
Affiliation:
1. U.S. Army Combat Capabilities Development Command Aviation & Missile Center, Ames Research Center, Moffett Field, California 94035
2. U.S. Army Combat Capabilities Development Command Army Research Laboratory, Hampton, Virginia 23666
Funder
Research, Development and Engineering Command
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035609
Reference17 articles.
1. Comparison of Aero-Propulsive Performance Predictions for Distributed Propulsion Configurations
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3. Parametric Study of Propeller Whirl Flutter Stability with Full-Span Model of X-57 Maxwell Aircraft
4. Whirl Flutter Analysis of a Free-Flying Electric-Driven Propeller Aircraft
5. ReedW. H. III, “Review of Propeller-Rotor Whirl Flutter,” NASA TR R-264, July 1967.
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