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[American Institute of Aeronautics and Astronautics AIAA Scitech 2020 Forum - Orlando, FL ()] AIAA Scitech 2020 Forum - Some effects of tunnel noise on cylinder-induced Mach 6 transitional shock wave boundary layer interactions
Leidy, Andrew, Neel, Ian T., Tichenor, Nathan R., Bowersox, Rodney D., Schmisseur, John D.DOI:
10.2514/6.2020-0582
File:
PDF, 1.80 MB