Flowfield of a Three-Dimensional Swept-Shock Boundary Layer Interaction at Mach 2

An experimental study is conducted on the interaction of a swept-shock wave with a turbulent boundary layer. The shock wave is generated by a sharp un-swept fin in a Mach 2 flow, where the strength of the interaction is varied from weak to moderate by changing the fin angle of attack fro...

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Bibliographic Details
Other Authors: Arora, Nishul (author)
Format: Others
Published: Florida State University
Online Access:http://purl.flvc.org/fsu/fd/2018_Fall_Arora_fsu_0071E_14877