机译:航天飞机轨道飞行器边界层/流线表面催化加热预测
b: bump factor equal to ratio of local catalytic to nominal heating rate; C_i: mass fraction of ith species; D_(ij): multicomponent diffusion coefficient; (e_ξ, _η, e_ζ): streamline coordinate-aligned unit vectors; H_(cl): arcjet nozzle centerline enthalpy, J/kg; H_w: wall enthalpy, J/kg; h°: enthalpy of formation, J/kg; h_(arc): heating parameter; (i, j, k): Cartesian-aligned unit vectors; L: Orbiter reference length, m; M_i: normal mass flux of ith species, kg/m~2 · s; P_(meas): measured test article surface pressure, N/m~2; q: heat flux per unit area, W/m~2; r: position vector, m; T: temperature, K; t: time, s; (u, v, w):Cartesian velocity components, m/s; V: velocity vector, m/s; (Xo,Yo,Zo): axial, lateral, and vertical shuttle coordinates,m; x: Orbiter axial distance from apex, m; (x,;
机译:X-34使用无粘性边界层方法的空气加热预测
机译:APS-流体动力学APS分部第70届年会-事件-流线矢量的定量及其在扫频冲击波/边界层相互作用(SBLI)的表面特征中的应用
机译:APS-流体动力学APS分部第70届年会-事件-流线矢量的定量及其在扫频冲击波/边界层相互作用(SBLI)的表面特征中的应用
机译:航天飞机轨道飞行器的BLIMPK /流线表面催化加热预测
机译:在空间穿梭球上的三维非平衡粘性激波层流动。
机译:湍流边界层结构研究在稀疏间隔的仿生脊柱覆盖的突出表面
机译:航天飞机轨道飞行器的BLIMPK /流线表面催化加热预测