机译:高超声速尖刺钝锥锥体的数值研究
A: area; m~2; A_f; A_b: frequency factor of forward; backward reaction; c: speed of sound; m/s; D: diameter of the dome of the nose cone; m; d: diameter of the aerodome; m; dp/dx: pressure gradient in the streamwise direction; dp/dy: pressure gradient normal to the wall; E: activation energy; H: altitude; km; L: length of the aerospike; m; M: Mach number; Pr: Prandtl number; P: pressure; N/m~2; q: heat flux; W/m~2; R: radius; m; Re_D: Reynolds number based on the diameter; T: temperature; K; U: velocity; m/s; u; v: streamwise; wall-normal velocity; m/s; x; y: streamwise; wall-normal direction; y ~+: nondimensional wall distance; α: separation angle of the recirculation area; deg; Δ_0: shock stand-off distance; m; ε: entropy fix; γ: ratio of specific heats; λ: eigenvalue; μ: viscosity; Ns/m~;
机译:高钝角锥上高超声速流动的数值模拟
机译:鼻尖钝性效应对锥体超声交叉流动性的实验研究
机译:零迎角小鼻钝的钝锥上高超声速边界层的稳定性分析和过渡预测
机译:超声波流过球形叶片的数值调查
机译:钝头体上的超音速粘性冲击层的理论和实验研究。
机译:粗糙元件对钝锥体上超声边界层的接受性的影响由于单频脉冲熵干扰
机译:高超声速流过钝头锥的马赫数为5.8的实验研究。