【摘 要】
:
Temporal mode direction numerical simulation has been done for the transition of a supersonic boundary layer on a flat plate with Mach number 4.5. Analysis of t
【机 构】
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DepartmentofMechanics,Liu-HuiCenterofAppliedMathematics,Liu-HuiCenterofAppliedMathematics
【基金项目】
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国家自然科学基金,the Foundation for the Author of National Excellent Doctoral Dissertation of China