Huang Hexia
Associate Professor
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Paper Publications
[1]黄河峡,.Flowfield induced by a plasma synthetic jet actuator with low exit inclination angle under low am....[J]:Aerospace Science and Technology
[2]黄河峡,.Flowfield of a helicopter submerged inlet with power output shaft.[J]:Acta Mechanica Sinica
[3]黄河峡,.Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios.[J].美国:AIAA Journal
[4]黄河峡,.带第三流路辅助进气的引射喷管流动特性研究.[J]:推进技术
[5]黄河峡,.亚声速S弯进气道研究的新进展.[J]:推进技术
[6]Huang Hexia,Tan Huijun,sz,张宇超,程林.Transient interaction between plasma jet and supersonic compression ramp flow.[J].American Institute of Physics:Physics of Fluids,2018
[7]黄河峡,谭慧俊,孙姝,凌棫.Evolution of supersonic corner vortex in a hypersonic inlet/isolator model.[J].American Institute of Physics:Physics of Fluids,2016
[8]Tan Huijun,,sz,Huang Hexia.Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves.[J]:Experiments in Fluids,2012
[9]Huang Hexia,Tan Huijun,sz,盛发家.Unthrottled Flows with Complex Background Waves in Curved Isolators.[J].The American Institute of Aeronautics and Astronautics:AIAA Journal,2017
[10]Huang Hexia,Tan Huijun,sz,王子运.Behavior of Shock Train in Curved Isolators with Complex Background Waves.[J].The American Institute of Aeronautics and Astronautics:AIAA Journal,2018
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