Flutter Predictions for Very Flexible Wing Wind Tunnel Test
Author:
Funder
Engineering and Physical Sciences Research Council
PAZY Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036710
Reference43 articles.
1. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs
2. T-tail flutter: Potential-flow modelling, experimental validation and flight tests
3. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future
4. Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
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