Effects of angle of attack and bluntness on heating rate distribution of blunt models at hypersonic speeds

DOI10.1134/S0015462819060090zbMath1434.76011OpenAlexW2996915785MaRDI QIDQ2181005

C. Senthilkumar, Singh Prakash Rampratap, G. Kadam Sunil, V. Shanmugam, M. Saiprakash, G. Balu

Publication date: 18 May 2020

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462819060090

zbMATH Keywords

heat transfer rateCFDsurface pressurehypersonic shock tunnelthin film platinum sensor

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Finite volume methods applied to problems in fluid mechanics (76M12) Hypersonic flows (76K05) Diffusive and convective heat and mass transfer, heat flow (80A19)

Related Items (1)

Skin friction reduction of hypersonic body by supersonic layer

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