Nonlinear Aeroelastic Analysis of High-Aspect-Ratio Wings with a Low-Order Propeller Model
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
2. Imperial College London, London, England SW7 2AZ, United Kingdom
Funder
Japan Society for the Promotion of Science
Casio Science Promotion Foundation
Mazda Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036285
Reference40 articles.
1. Propeller Effects on the Response of High-Altitude Long-Endurance Aircraft
2. Dynamic Response of Highly Flexible Flying Wings
3. Gust Response for Flexibly Suspended High-Aspect Ratio Wings
4. Application of a panel code to unsteady wing-propeller interference
5. Aerodynamic interaction between propellers and wings
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