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Investigation on design method of curved compression surface of inlet on scramjet
MATEC Web of Conferences
Suppose that curved compression surface of inlet consists of segments. Two curved surfaces formed by equal compression angles of the micro-element segments and a slight increase in the compression angle of the micro-element segments are designed respectively. The numerical simulation method is used to compare the performance of two curved surfaces with the reference three-wedge compression surface. Select NASA classic test data, in order to determine the turbulence model and calculation methoddoi:10.1051/matecconf/202235501001 fatcat:7y63agvwlzcs7hiss4khl6nupm