High-pressure layer generation in a compression corner at a supersonic flow velocity

DOI10.1134/S0015462814060131zbMath1308.76156OpenAlexW1993481089MaRDI QIDQ2019032

I. I. Lipatov, V. I. Zapryagaev, I. N. Kavun

Publication date: 26 March 2015

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

Full work available at URL: https://doi.org/10.1134/s0015462814060131

zbMATH Keywords

supersonic flowshock wavesseparationcompression corner

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (1)

Compact quasi-gas-dynamic system and high performance computing

Cites Work

• Shock Wave-Boundary-Layer Interactions
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