Huang Hexia
Associate Professor
Supervisor of Doctorate Candidates
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黄河峡.Flowfield induced by a plasma synthetic jet actuator with low exit inclination angle under low ambient pressure.Aerospace Science and Technology
黄河峡.Flowfield of a helicopter submerged inlet with power output shaft.Acta Mechanica Sinica
黄河峡.Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios.AIAA Journal
黄河峡.带第三流路辅助进气的引射喷管流动特性研究.推进技术
黄河峡.亚声速S弯进气道研究的新进展.推进技术
Huang Hexia.Transient interaction between plasma jet and supersonic compression ramp flow.Physics of Fluids.2018
Patents
一种矩形高超声速进气道的内通道型面设计方法
一种高超声速内转式进气道的内通道设计方法
一种适用于超声速/高超声速流道的流量测试系统及测试方法
基于流线偏折的高超声速内转式进气道唇罩设计方法
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