Time-Dependent Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors
Author:
Affiliation:
1. University of Rome, 00146 Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.4817
Reference20 articles.
1. 2Nixon, M. W. "Aeroelastic Response and Stability of Tiltrotors with Elastically-Coupled Composite Rotor Blades," Ph.D. Dissertation, Dept. of Aerospace Engineering,Universityof Maryland,College Park, MD,1993.
2. Aeroelastic Analysis of Advanced Geometry Tiltrotor Aircraft
3. Validation of a Comprehensive Aeroelastic Analysis for Tiltrotor Aircraft
4. Aeroelastic Tailoring for Stability Augmentation and Performance Enhancements of Tiltrotor Aircraft
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