Input-output analysis of complex hypersonic boundary layers

作者: Joseph W. Nichols , Graham V. Candler

DOI: 10.2514/6.2019-1383

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参考文章(11)
Robert W. MacCormack, Numerical computation of compressible and viscous flow American Institute of Aeronautics and Astronautics, c2014. ,(2014) , 10.2514/4.102646
Alexander V. Fedorov, Andrew P. Khokhlov, Prehistory of Instability in a Hypersonic Boundary Layer Theoretical and Computational Fluid Dynamics. ,vol. 14, pp. 359- 375 ,(2001) , 10.1007/S001620100038
Boa-Teh Chu, On the energy transfer to small disturbances in fluid flow (Part I) Acta Mechanica. ,vol. 1, pp. 215- 234 ,(1965) , 10.1007/BF01387235
B. J. McKeon, A. S. Sharma, I. Jacobi, Experimental manipulation of wall turbulence: a systems approach Physics of Fluids. ,vol. 25, pp. 031301- ,(2013) , 10.1063/1.4793444
M. R. Malik, R. E. Spall, On the stability of compressible flow past axisymmetric bodies Journal of Fluid Mechanics. ,vol. 228, pp. 443- 463 ,(1991) , 10.1017/S002211209100277X
Shann Rufer, Steven Schneider, HOT-WIRE MEASUREMENTS OF INSTABILITY WAVES ON A BLUNT CONE AT MACH-6 35th AIAA Fluid Dynamics Conference and Exhibit. ,(2005) , 10.2514/6.2005-5137
Alexander Fedorov, Transition and Stability of High-Speed Boundary Layers Annual Review of Fluid Mechanics. ,vol. 43, pp. 79- 95 ,(2011) , 10.1146/ANNUREV-FLUID-122109-160750
David A. Cook, John Thome, Joseph M. Brock, Joseph W. Nichols, Graham V. Candler, Understanding effects of nose-cone bluntness on hypersonic boundary layer transition using input-output analysis 2018 AIAA Aerospace Sciences Meeting. ,(2018) , 10.2514/6.2018-0378
Anthony Knutson, Sidharth Gs, Graham V. Candler, Instabilities in mach 6 flow over a cone with a swept fin 48th AIAA Fluid Dynamics Conference, 2018. ,(2018) , 10.2514/6.2018-3071