RANS Modelling of Shock-Wave Boundary Layer Interaction in a Mixed Compression Axisymmetric Hypersonic Intake

Publisher: Trans Tech Publications

E-ISSN: 1662-7482|2016|846|61-66

ISSN: 1660-9336

Source: Applied Mechanics and Materials, Vol.2016, Iss.846, 2016-09, pp. : 61-66

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Abstract