Receptivity and Stability Theory Analysis of a Transonic Swept Wing Experiment
Yuanqiang Liu,
Yan Liu,
Zubi Ji
et al.
Abstract:Surface suction provides an efficient way to delay boundary layer transitions. In order to verify the suction effects and determine the mechanism of suction control in transonic swept wing boundary layers, wind tunnel transition measurements in a hybrid laminar flow control (HLFC) wind tunnel model uses an infrared thermography technique in the Aircraft Research Association (ARA) 2.74 m × 2.44 m low turbulence level transonic wind tunnel. Based on the experimental data of stationary crossflow dominant transiti… Show more
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