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521.
A numerical investigation on jet interaction in supersonic laminar flow with a compres- sion ramp is performed utilizing the AUSMDV scheme and a parallel solver. Several parameters dominating the interference flowfield are studied after defining the relative increment of normal force and the jet amplification factor as the evaluation criterion of jet control performance. The computational results show that most features of the interaction flowfield between the transverse jet and the ramp are similar to those between a jet and a flat plate, except that the flow structures are more complicated and the low-pressure region behind the jet is less extensive. The relative force increment and the jet amplification factor both increase with the distance between the jet and the ramp shortening till quintuple jet diameters. Inconspicuous difference is observed between the jet-before-ramp and jet-on-ramp cases. The variation of the injection angle changes the extent of the separation region, the plateau pressure, and the peak pressure near the jet. In the present computational conditions, 120 is indicated relatively optimal among all the injection angles studied. For cold gas simulations, although little influence of the jet temperature on the pressure distribution near the jet is observed under the computation model and the flow parameters studied, reducing jet temperature somehow benefits the improvement of the normal force and the jet efficiency. When the pressure ratio of jet to freestream is fixed, the relative force increment varies little when increasing the freestream Mach number, while the jet amplification factor increases. 相似文献
522.
基于一种简化的平衡分布函数,提出一种新的动理学通量矢量分裂(KineticFluxVectorSplitting,KFVS)格式来求解Euler方程。算例证实,新的KFVS格式继承了原始KFVS格式中捕捉激波准确、无数值震荡的优点。与原始的KFVS格式相比,由于简化的平衡分布函数与Maxwellian平衡分布函数相比复杂程度大大降低,计算中不需要再计算误差函数,新的KFVS格式的计算效率得到了很大提高。在同样的计算精度下,新KFVS格式比原始KFVS格式计算效率提高了一倍以上,显示了新格式具有良好的数值模拟性能。 相似文献
523.
524.
采用相对论平均场理论(RMFT)下的GL85,GL92,TM1和TM2等核物质参数组,研究了这些参数组对中子星的粒子数密度分布、状态方程及质量-半径关系的影响.结果表明,在不同的参数组下,超子出现的密度、顺序和种类均不同;状态方程的软硬情况也较大不同;中子星的引力质量和相应的半径有明显不同.计算结果也表明,采用GL85,TM1和TM2等参数组得到的中子星质量和半径均在脉冲星的观测数据范围内,而采用GL92参数组得到的中子星质量小于中子星质量下限1.4M⊙(M⊙=1.99×1030kg为太阳质量). 相似文献
525.
《中国航空学报》2016,(6):1553-1562
This paper deals with the numerical solution of inviscid compressible flows. The threedimensional Euler equations describing the mentioned problem are presented and solved numerically with the finite volume method. The evaluation of the numerical flux at the interfaces is performed by using the Toro Vazquez-Harten Lax Leer(TV-HLL) scheme. An essential feature of the proposed scheme is to associate two systems of differential equations, called the advection system and the pressure system. It can be implemented with a very simple manner in the standard finite volume Euler and Navier–Stokes codes as extremely simple task. The scheme is applied to some test problems covering a wide spectrum of Mach numbers, including hypersonic, low speed flow and three-dimensional aerodynamics applications. 相似文献
526.
S.A. Elwakil E.M. Abulwafa E.K. El-Shewy H.M. Abd-El-Hamid 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
A theoretical investigation has been made for electron acoustic waves propagating in a system of unmagnetized collisionless plasma consists of a cold electron fluid and ions with two different temperatures in which the hot ions obey the non-thermal distribution. The reductive perturbation method has been employed to derive the Korteweg–de Vries equation for small but finite amplitude electrostatic waves. It is found that the presence of the energetic population of non-thermal hot ions δ, initial normalized equilibrium density of low temperature ions μ and the ratio of temperatures of low temperature ions to high temperature ions β do not only significantly modify the basic properties of solitary structure, but also change the polarity of the solitary profiles. At the critical hot ions density, the KdV equation is not appropriate for describing the system. Hence, a new set of stretched coordinates is considered to derive the modified KdV equation. In the vicinity of the critical hot ions density, neither KdV nor modified KdV equation is appropriate for describing the electron acoustic waves. Therefore, a further modified KdV equation is derived. An algebraic method with computerized symbolic computation, which greatly exceeds the applicability of the existing tanh, extended tanh methods in obtaining a series of exact solutions of the various KdV-type equations, is used here. Numerical studies have been reveals different solutions e.g., bell-shaped solitary pulses, singular solitary “blowup” solutions, Jacobi elliptic doubly periodic wave, Weierstrass elliptic doubly periodic type solutions, in addition to explosive pulses. The results of the present investigation may be applicable to some plasma environments, such as Earth’s magnetotail region. 相似文献
527.
树脂炭化是一个复杂的物理化学变化过程,包括传热传质、应力应变、热分解等耦合过程。基于物理守恒原理,理论推导出了瞬态的热-流-固耦合方程组,包括树脂变形方程、热解气体渗流方程和能量守恒方程,分析了各物理场之间的相互耦合作用,并对后续研究提出建议。 相似文献
528.
提出了一种优化风力机翼型气动特性的设计方法。在现有风力机翼型的基础上,通过改变其最大厚度位置至后缘部分的外形进行优化计算。采用N-S方程计算翼型的流场及气动特性,以提高风力机切向力同时减小其法向力为目的,用二维线性插值的方法进行多目标优化。以DU 93W 210翼型为例,针对风力机翼型气动性能本身的矛盾性,根据实际需求提出几种方案加以优化。结果表明,在不同的性能需求下,本文所提出的设计方法能取得较好的效果。 相似文献
529.
采用对比分析的方法,对求解可压缩流动的低耗散E-CUSP(LDE)迎风格式的性能进行测评,目的是进一步更好地将其用于分离涡数值模拟。对比格式采用广泛使用的Roe格式。控制方程为Euler和雷诺平均Navier-Stokes方程耦合Spalart-Allmaras一方程湍流模型,采用全隐式无分裂Gauss-Seidel线松驰时间推进方法。结果表明,LDE格式具有强的捕捉激波能力,计算结果与Roe格式一致,和实验数据吻合良好。相对于Roe格式,LDE格式具有较快的收敛速度。 相似文献
530.