【摘 要】
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The hypersonic boundary-layer receptivity to slow acoustic waves is investigated for the Mach 6 flow over a 5-degree half-angle blunt cone with the nose radius
【机 构】
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LaboratoryforHigh-SpeedAerodynamics
【基金项目】
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Project supported by the National Natural Science Foundation of China(Nos.11472188 and 11332007)and the National Key Research and Development Program of China(No.2016YFA0401200).