Open AccessEffects of Upstream Disturbances on Supersonic Flowfield with Transverse Injection
Author(s) -
Shohei URAMOTO,
Toshinori Kouchi,
Goro Masuya
Publication year - 2016
Publication title -
journal of the japan society for aeronautical and space sciences
Language(s) - English
Resource type - Journals
eISSN - 2432-3691
pISSN - 1344-6460
DOI - 10.2322/jjsass.64.244
Subject(s) - mach number , oblique shock , boundary layer , supersonic speed , mechanics , physics , shock wave , transverse plane , bow shock (aerodynamics) , wake , shock (circulatory) , jet (fluid) , boundary layer thickness , mach wave , stagnation point , optics , structural engineering , engineering , medicine , heat transfer
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