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机译:超音速进气道绕过环形通道的流动模拟
NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135, Ohio Aerospace Institute, 22800 Cedar Point Road, Cleveland, OH 44142;
rnNASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135;
rnNASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135;
rnNASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135;
rnGulfstream Aerospace Corporation, Savannah, Georgia 31402;
A: area; AIP: aerodynamic interface plane, engine fan face; B: blockage; TPR: total pressure recovery; MFR: mass-flow rate, m; P_b: backpressure;
机译:超音速进气道绕过环形通道的流动模拟
机译:进气道节流时超音速流动破坏的数值研究
机译:具有入口压缩坡道的氢射流进入超音速错流燃烧室的反应流的大涡模拟
机译:带有支撑杆和环形旁通管的轴对称超声速进气道的流动模拟
机译:通过替代模型对轴对称超音速进气旁路分流器进行多目标优化。
机译:超声分离过程中进,出口流动条件对天然气参数的影响
机译:超声波流动空气动力滞后在轴对细胞上的空气动力滞后流量控制的数值模拟
机译:带旁路环形管的超音速进气道流动模拟