Measurement and Identification of Supersonic Stationary Crossflow Waves Based on Sublimation Method
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DOI: 10.2514/1.j062571
Abstract: Aiming at the crossflow transition problem of supersonic swept wings, an experimental study on the measurement and identification of boundary-layer stationary crossflow waves was carried out at Mach number 2.0. A 65 deg straight-swept-wing model with… read more here.
Keywords: sublimation; crossflow; crossflow waves; measurement identification ... See more keywords