Effect of shock impingement location on the fluid–structure interactions over a compliant panel
Author:
Funder
Defense Sciences Office, DARPA
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00193-024-01162-9.pdf
Reference26 articles.
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2. Touber, E., Sandham, N.D.: Low-order stochastic modelling of low-frequency motions in reflected shockwave/boundary-layer interactions. J. Fluid Mech. 671, 417–465 (2011). https://doi.org/10.1017/S0022112010005811
3. Liuqing, Y.E., Zhengying, Y.E., Xiochen, W.: Aeroelastic stability analysis of heated flexible panel subjected to an oblique shock. Chin. J. Aeronaut. 31(8), 1650–1666 (2018). https://doi.org/10.1016/j.cja.2018.05.019
4. Casper, K.M.: Fluid–structure interactions on a slender cone under quiet flow conditions at Mach 6. 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Grapevine, TX, AIAA Paper 2017-0402 (2017). https://doi.org/10.2514/6.2017-0402
5. Maestrello, L.: Design criterion of panel structure excited by turbulent boundary layer. J. Aircr. 5(4), 321–328 (1968). https://doi.org/10.2514/3.43946
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