机译:超音速流动下菱形喷油嘴的实验与数值研究
Japan Aerospace Exploration Agency, Tsukuba 305-8505, Japan Space Transportation Mission Directorate, Ibaraki;
rnTexas A&M University, College Station, Texas 77843 Aerospace Engineering;
rnTexas A&M University, College Station, Texas 77843 Aerospace Engineering currently Ramgen Power Systems, LLC;
rnTexas A&M University, College Station, Texas 77843 Graduate Research Assistant, Aerospace Engineering;
rnU.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433 Aerospace Propulsion Division;
rnUniversal Technology Corporation, Dayton, Ohio 45432 Aerospace Propulsion Division;
ER: fuel-oxygen equivalence ratio; J: jet-to-freestream dynamic pressure ratio, (ρu~2)_(jet)/(ρu~2)_(freestream); P_s: gas static pressure; P_0: gas total pressure; T_s: gas static temperature;
机译:超音速流动下菱形喷油嘴的实验与数值研究
机译:通过壁向超音速射流加热和冷流的气体动力学相互作用的实验和数值研究
机译:级联喷油器在超音速流中引起的混合增强机理:数值研究
机译:超音速流量中菱形注射器的研究(邀请呈现)
机译:超音速流在二维钻石形翼型上能量沉积的数值研究。
机译:超音速腔流动的数值激光能量沉积和控制流动的传感器放置策略
机译:喷射喷射进入多孔腔的超音速主流的数值研究