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Published in 2018 at "SIMULATION"
DOI: 10.1177/0037549717733051
Abstract: The present work provides a detailed comparative study of the hypersonic flow past spherically blunted and parabolic nose cones at a Mach number of 5.8, numerically. The main focus of the paper is to determine…
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Keywords:
hypersonic flow;
comparative study;
drag;
parabolic nose ... See more keywords