Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter
Author:
Affiliation:
1. Ames Research Center, Moffett Field, California 94035
2. Army Research Laboratory, Aberdeen, Maryland 21005
3. Army Research Laboratory, Hampton, Virginia 23666
Funder
U.S. Army Combat Capabilities Development Command
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036950
Reference28 articles.
1. Prop‐Rotor Stability at High Advance Ratios
2. ReedW. H. III, “Review of Propeller-Rotor Whirl Flutter,” NASA TR R-264, July 1967.
3. The Effect of Positive Pitch-flap Coupling (Negative δ3) on Rotor Blade Motion Stability and Flapping
4. JohnsonW. “Dynamics of Tilting Proprotor Aircraft in Cruise Flight,” NASA TN D-7677, May 1974.
5. JohnsonW. “Analytical Modeling Requirements for Tilting Proprotor Aircraft Dynamics,” NASA TN D-8013, July 1975.
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