Stall Flutter of the Benchmark Supercritical Wing at High Angles of Attack
Author:
Affiliation:
1. Technion Israel Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0760
Reference23 articles.
1. EXPERIMENTAL UNSTEADY PRESSURES AT FLUTTER ON THE SUPERCRITICAL WING BENCHMARK MODEL
2. A new forced oscillation capability for the Transonic Dynamics Tunnel
3. Experimental data from the Benchmark SuperCritical Wing wind tunnel test on an oscillating turntable
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