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   超声速流动 的翻译结果: 查询用时:0.649秒
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      超声速流动
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  supersonic flow
     Hybrid RANS / LES simulation of the supersonic flow over two-dimensional cavities
     二维凹腔超声速流动的混合RANS/LES模拟
短句来源
     The flow visualization technique using shear-sensitive liquid crystal is applied to the investigation of a Mach 2 internal supersonic flow with pseudo-shock wave (PSW) in a pressure-vacuum supersonic wind tunnel.
     在一个压力-真空超声速风洞中,剪切应力敏感液晶流动可视化技术被应用来研究方管内马赫数2拟似冲击波(pseudo shockwave)的超声速流动
短句来源
     The region marching method for supersonic flow and the time iteration method for N-S equations and space marching method for PNS equations were introduced.
     介绍了超声速流场的分区推进求解技术、流动的时间迭代和超声速流动的空间推进求解方法。
短句来源
     Local overheat causing by the protuberance on the surface of reentry spacecraft in the condition of hypersonic and supersonic flow is discussed briefly.
     阐述了高超声速和超声速流动条件下, 返回式航天器防热层表面的突起物所引起局部过热问题; 分析了突起物对其周围防热层表面的局部热环境的影响及其本身表面所处的热环境。
短句来源
     A calculation for the two-dimensional supersonic flow in an angle-shaped tube is presented by using the Euler equations and the implicit TVD (Total Variation Diminishing) scheme. A multigrid algorithm is designed to make more effective modeling of the interaction and reflection of shock waves and rarefaction waves on a body surface.
     本文应用Euler模型和隐式TVD格式计算了二维折角管道内的超声速流动问题,为了有效地模拟激波和膨胀波系的相互干扰及壁面的反射,本文试将多重网格法和TVD格式结合起来进行数值求解。
短句来源
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  supersonic flows
     Study on Internal Supersonic Flows with Pseudo-shock Wave Using Liquid Crystal Flow Visualization Method
     液晶流动可视化方法研究拟似冲击波的内部超声速流动(英文)
短句来源
     A number of numericalIv com-puted examples on the airfoils at transonic and supersonic flows demon-strate that the present method shows better stability and suppresses effec-tively the oscillation on both sides of the shock.
     对翼型的跨超声速流动算例表明,本法具有较好的稳定性和能有效地抑制激波两侧振荡。
短句来源
     Eight popular nonlinear turbulence models under lowRe kε framework have been tested and validated against experimental data of two supersonic flows with shock-wave/ boundary-layer interaction including separation.
     本文在低雷诺数k-ε两方程框架下,应用八个常见的非线性湍流模式,对两个激波/边界层相互作用诱导分离的超声速流动进行了研究。
短句来源
     A numerical simulation is presented for the steady state flow for transonic and supersonic flows. We integrated numerically the 3 D Reynolds averaged Navier Stokes equations, using central finite volume method and explicit Runge Kutta algorithm on the basis of one of three turbulent models: B L(Baldwin Lomax) model, J K90A model or J K92 model.
     采用中心有限体积、Runge- Kutta方法显式求解三维 Reynolds平均 Navier- Stokes方程 ,使用三种湍流模型数值模拟跨声速及超声速流动
短句来源
     Rarefaction effect tends to make supersonic flows move smoothly, and to enlarge the influence domain of cylinder.
     稀薄效应趋于弱化激波等超声速流动结构,物体影响域增大。
短句来源
  “超声速流动”译为未确定词的双语例句
     A MULTIGRID CALCULATION FOR THE TWO-DIMENSIONAL SUPERSONIC FLOW IN AN ANGLE-SHAPED TUBE
     二维折角管道内超声速流动的多重网格计算
短句来源
     On the Favorable Interference in the Supersonic Flow
     论超声速流动中的有益干扰
短句来源
     Effecting parameters of supersonic flowfield with secondary injection
     超声速流动中横向射流流场的影响参数
短句来源
     In this paper, we based on the analysis of the grid Reynolds numbers R Δ x i , applied the couple discrete fluid theory (CDFT) to practical computation, simulated the supersonic separated flows of rearward\|facing step and got some meaningful results.
     本文通过离散单元上网格雷诺数的变化分析 ,采用耦合离散流体理论 (CDFT)差分格式 ,对向后台阶底部超声速流动问题进行数值模拟 ,得到了满意的结果。
短句来源
     The configurations consist of a 20°compression corner and an axisymmetric ogive-cylinder-flare.
     两个超声速流动为:20°可压缩拐角绕流和轴对称尖顶拱-柱-裙组合体绕流。
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  supersonic flow
A singularly perturbed problem for stable supersonic flow
例句来源      
Numerical solution of the problem of supersonic flow past conical bodies at an angle of attack
例句来源      
The case is studied when the wing velocity is supersonic and its edges satisfy the supersonic flow condition.
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Unsteady supersonic flow around blunt bodies with detached shock wave
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The hypersonic similarity laws for flow around slender blunt bodies [1-3] are generalized to bodies with nonsmooth lateral surface, in particular, those having corners (under the condition of unseparated supersonic flow).
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  supersonic flows
In this paper it is shown that, with the aid of the stream surfaces of supersonic flows past cones at zero angle of attack, one can construct a quite broad class of bodies whose shape and aerodynamic characteristics are easily computed.
例句来源      
Calculating base pressures in two-dimensional supersonic flows
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A general method is described for determining the base pressure in complex two-dimensional supersonic flows.
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The recently initiated study of steady-state supersonic flows of combustible gaseous mixtures with the occurrence of detonation waves and slow-combustion fronts is the result of several factors.
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Method for calculating two-dimensional supersonic flows of a chemically reacting inviscid gas
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