Analysis of Limit Cycle Oscillation Data from the Aeroelastic Test of the SUGAR Truss-Braced Wing Model
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2720
Reference10 articles.
1. Computed and Experimental Flutter/LCO Onset for the Boeing Truss-Braced Wing Wind Tunnel Model
2. SUGAR Truss Braced Wing Full Scale Aeroelastic Analysis and Dynamically Scaled Wind Tunnel Model Development
3. Aeroservoelastic Wind-Tunnel Test of the SUGAR Truss Braced Wing Wind-Tunnel Model
4. Transport Wing Flutter Model Transonic Limit Cycle Oscillation Test
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Designing high aspect ratio wings: A review of concepts and approaches;Progress in Aerospace Sciences;2024-02
2. Aeroservoelastic Test of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Model;Journal of Guidance, Control, and Dynamics;2016-08
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