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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059369
Abstract: Experimental studies are carried out to investigate the effects of the geometrical parameters with a drag reducing spike on a hemispherical forebody in a supersonic freestream of M∞=2.0 at 0 deg an...
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Keywords:
supersonic flow;
studies supersonic;
flow unsteadiness;
unsteadiness hemispherical ... See more keywords