Transition control of Mach 6.5 hypersonic flat plate boundary layer

An artificial disturbance is introduced into the boundary layer over a flat plate to investigate the effect on the transition process in the Mach 6.5 wind tunnel at Peking University. A linear stability theory (LST) is utilized to predict the evolution of the eigenmodes, and the frequency of the art...

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Veröffentlicht in:	Applied mathematics and mechanics 2019-02, Vol.40 (2), p.283-292
Hauptverfasser:	Zhang, Yunchi, Li, Chi
Format:	Artikel
Sprache:	eng
Schlagworte:	Applications of Mathematics Boundary layer stability Boundary layer transition Classical Mechanics Disturbances Flat plates Fluid- and Aerodynamics Instability waves (fluids) Mathematical Modeling and Industrial Mathematics Mathematics Mathematics and Statistics Partial Differential Equations Particle image velocimetry Stability Velocity measurement Wind tunnels
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