Influence of hypersonic fluid-structure interaction on the control authority of a trailing-edge flap
Author:
Affiliation:
1. University of New South Wales at the Australian Defence Force Academy
2. University of Southern Queensland
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5265
Reference33 articles.
1. Numerical study of the influence of non-uniform wall temperature distribution on the hypersonic flow over a flat plate
2. Bhattrai, S., de Baar, J. H., and Neely, A. J. “Efficient uncertainty quantification for a hypersonic trailing-edge flap, using gradient-enhancedkriging,”AerospaceScienceandTechnology,2018.
3. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
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