Huang Hexia
Associate Professor
Supervisor of Doctorate Candidates
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[11]Huang Hexia,Tan Huijun,sz,宁乐,王娇.Characterization of Two Typical Unthrottled Flows in Hypersonic Inlet/Isolator Models.[J].American Institute of Aeronautics and Astronautics:Journal of Aircraft,2015
[12]Huang Hexia,Tan Huijun,庄逸,盛发家,sz.高超声速进气道/隔离段内流特性研究进展.[J].北京:推进技术,2018
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