Effect of Wall Suction and Cooling on the Stability of the Supersonic and Hypersonic Three Dimensional Boundary Layer[J]. ACTA AERODYNAMICA SINICA, 1999, 17(1): 21-29.
Citation:
Effect of Wall Suction and Cooling on the Stability of the Supersonic and Hypersonic Three Dimensional Boundary Layer[J]. ACTA AERODYNAMICA SINICA, 1999, 17(1): 21-29.
Effect of Wall Suction and Cooling on the Stability of the Supersonic and Hypersonic Three Dimensional Boundary Layer[J]. ACTA AERODYNAMICA SINICA, 1999, 17(1): 21-29.
Citation:
Effect of Wall Suction and Cooling on the Stability of the Supersonic and Hypersonic Three Dimensional Boundary Layer[J]. ACTA AERODYNAMICA SINICA, 1999, 17(1): 21-29.
Effect of Wall Suction and Cooling on the Stability of the Supersonic and Hypersonic Three Dimensional Boundary Layer
In the paper the fourth order accurate scheme is used to study the effect of wall suction and cooling on the cross flow instability of a supersonic and hypersonic three dimensional boundary layer．The maximum Mach number is as high as M＝7．5．The numerical r
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