Computational analysis of the aerothermodynamic effects in a reentry vehicle with surface discontinuity like a combined GAP/STEP
This work is a computational study of a hypersonic rarefied non-reacting flow past a combined gap/step configuration at zero-degree angle of attack in thermal nonequilibrium conditions. Effects on the flowfield structure and on the aerodynamic surface quantities due to changes in the gap L/H ratio a...
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| Language: | English |
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Instituto Nacional de Pesquisas Espaciais (INPE)
2015
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| Online Access: | http://urlib.net/sid.inpe.br/mtc-m21b/2015/06.09.17.32 |