@inproceedings{tumuklu2024a,
	title = {Effect of {Spanwise} {Instabilities} on {Hypersonic} {Flows}},
	doi = {10.2514/6.2024-3834},
	abstract = {This study investigates hypersonic Mach 7.1 flows with varying unit Reynolds numbers of 5.2E+4, 1.04E+5, and 4.14E+5 1/m over a double wedge with wedge angles of 0/30◦, 5/30◦, and 30/45◦ using both 2D and 3D configurations. Significant influences of wedge angles on shock interactions, flow dynamics, and surface parameters are observed. A detailed analysis of the temporal characteristics of the flow and surface fields is carried out. The characteristics of self-induced spanwise instabilities in the relatively large separation region are closely examined. Increasing the wedge angles led to a nonlinear increase in spanwise instabilities.},
	urldate = {2024-09-16},
	booktitle = {{AIAA} {AVIATION} {FORUM} {AND} {ASCEND} 2024},
	publisher = {AIAA Paper 2024-3834},
	author = {Tumuklu, Ozgur},
	year = {2024},
	doi = {10.2514/6.2024-3834},
	note = {\_eprint: https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3834},
}

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