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机译:小型超音速进气口的流动特性
PGM Research and Development Laboratory Seoul National University, School of Mechanical and Aerospace Engineering, Seoul 151-742, Republic of Korea LIG Nexl, Co., Ltd., Daejeon 305-804, Republic of Korea;
PGM Research and Development Laboratory Seoul National University, School of Mechanical and Aerospace Engineering, Seoul 151-742, Republic of Korea LIG Nexl, Co., Ltd., Daejeon 305-804, Republic of Korea;
Seoul National University, School of Mechanical and Aerospace Engineering, Seoul 151 -742, Republic of Korea Seoul National University, Seoul 151-742, Republic of Korea;
Department of Aerospace Engineering, Institute of Advanced Aerospace Technology Seoul National University, Seoul 151-742, Republic of Korea;
A_e: geometrical throat area of exit jet; A_t: cross-sectional area at throat section of inlet; Ai: cross-sectional area at entrance of test model; c: speed of sound; f_n: fundamental frequency of inlet buzz;
机译:小型超音速进气口的流动特性
机译:进气湍流对通过具有超声速进气道的叶尖截面涡轮叶片叶栅的可压缩流的影响
机译:带隔离器的超音速入口超音速流中超音速薄膜冷却的数值分析
机译:二维混合压缩超音速入口入口的非定常流动特性
机译:超声速入口中次生流体对激波/边界层相互作用引起的流动分离的作用。
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:隔离器超音速入口在超音速入口处的超音速膜冷却的数值分析
机译:一个环形超音速进气道零速飞行的一些内部流动特性以及带有尖锐和圆形唇形的开口进气口