机译:超音速加热计算的欧拉通量评估
Japan Aerospace Exploration Agency, Kanagawa 229-8510, Japan Engineering Digital Innovation Center, 3-1-1 Yoshinodai, Sagamihara;
rnJapan Aerospace Exploration Agency, Kanagawa 229-8510, Japan Team for Utilization of Simulation Technology, Engineering Digital Innovation Center, 3-1-1 Yoshinodai, Sagamihara;
rnNagoya University, Aichi 464-8603, Japan Department of Aerospace Engineering, 1 Furo-cho, Chikusaku, Nagoya;
rnUniversity of Michigan, Ann Arbor, Michigan 48109-2140 Department of Aerospace Engineering;
AR: cell aspect ratio; C_p: specific heat at constant pressure; E: total energy; E, F: inviscid flux vectors (in x, y directions, respectively); E_v, F_v: viscous flux vectors (in x, y directions, respectively);
机译:超音速加热计算的欧拉通量评估
机译:超音速流动计算的欧拉通量评估
机译:非平衡高超声速流的耦合Euler /缺陷边界层与Navier-Stokes计算之间的比较
机译:欧拉通量的评估II:高超声速表面加热计算
机译:纳米流体在加热和冷却强制对流应用中的计算与实验评价
机译:通过低成本旋转传感器数据提高欧拉角计算的精度和速度
机译:超音速进气流中壁面热通量的计算
机译:高超声速条件下表面催化加热的综合实验与计算研究。