Novel Method Based on Inflatable Bump for Vertical Tail Buffeting Suppression
Author:
Affiliation:
1. School of Aerodynamics, Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032552
Reference12 articles.
1. Vertical tail buffeting of fighter aircraft
2. Research into vortex breakdown control
3. Controlled Vortex Breakdown on Modified Delta Wings
4. A Method of Inflatable Leading Edge for High Lift,Deicing and Noise Reduction
5. Aircraft anti-icing and de-icing techniques and modeling
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1. Aerodynamic Exploration of Corrugated Airfoil Based on NACA0030 for Inflatable Wing Structure;Aerospace;2023-02-13
2. Study on influence of ambient temperature on biaxial stress and strength of flexible inflatable wing film;Results in Physics;2019-03
3. Study on modal properties of flexible inflatable wing skin film structure;Journal of Physics: Conference Series;2018-07
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