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Investigation of Navier-Stokes code verification and design optimization.

机译:Navier-Stokes代码验证和设计优化研究。

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With rapid progress made in employing computational techniques for various complex Navier-Stokes fluid flow problems, design optimization problems traditionally based on empirical formulations and experiments are now being addressed with the aid of computational fluid dynamics (CFD). To be able to carry out an effective CFD-based optimization study, it is essential that the uncertainty and appropriate confidence limits of the CFD solutions be quantified over the chosen design space. The present dissertation investigates the issues related to code verification, surrogate model-based optimization and sensitivity evaluation.; For Navier-Stokes (NS) CFD code verification a least square extrapolation (LSE) method is assessed. This method projects numerically computed NS solutions from multiple, coarser base grids onto a finer grid and improves solution accuracy by minimizing the residual of the discretized NS equations over the projected grid. In this dissertation, the finite volume (FV) formulation is focused on. The interplay between the concepts and the outcome of LSE, and the effects of solution gradients and singularities, nonlinear physics, and coupling of flow variables on the effectiveness of LSE are investigated.; A CFD-based design optimization of a single element liquid rocket injector is conducted with surrogate models developed using response surface methodology (RSM) based on CFD solutions. The computational model consists of the NS equations, finite rate chemistry, and the k-epsilonturbulence closure. With the aid of these surrogate models, sensitivity and trade-off analyses are carried out for the injector design whose geometry (hydrogen flow angle, hydrogen and oxygen flow areas and oxygen post tip thickness) is optimized to attain desirable goals in performance (combustion length) and life/survivability (the maximum temperatures on the oxidizer post tip and injector face and a combustion chamber wall temperature). A preliminary multi-objective optimization study is carried out using a geometric mean approach. Following this, sensitivity analyses with the aid of variance-based non-parametric approach and partial correlation coefficients are conducted using data available from surrogate models of the objectives and the multi-objective optima to identify the contribution of the design variables to the objective variability and to analyze the variability of the design variables and the objectives.; In summary the present dissertation offers insight into an improved coarse to fine grid extrapolation technique for Navier-Stokes computations and also suggests tools for a designer to conduct design optimization study and related sensitivity analyses for a given design problem.
机译:随着在针对各种复杂的Navier-Stokes流体流动问题采用计算技术方面取得快速进展,传统上基于经验公式和实验的设计优化问题现在正借助计算流体动力学(CFD)来解决。为了能够进行有效的基于CFD的优化研究,至关重要的是,必须在选定的设计空间内对CFD解决方案的不确定性和适当的置信度进行量化。本文研究了与代码验证,替代基于模型的优化和敏感性评估有关的问题。对于Navier-Stokes(NS)CFD代码验证,评估了最小二乘外推(LSE)方法。该方法将数值计算的NS解从多个更粗糙的基础网格投影到更精细的网格上,并通过最小化投影网格上离散NS方程的残差来提高求解精度。本文重点研究了有限体积法。研究了LSE的概念和结果之间的相互作用,以及溶液梯度和奇异性,非线性物理学以及流量变量耦合对LSE有效性的影响。使用基于CFD解决方案的响应面方法(RSM)开发的替代模型,对单元素液体火箭喷射器进行了基于CFD的设计优化。该计算模型由NS方程,有限速率化学和k-ε湍流闭合组成。借助这些替代模型,对喷射器设计进行了灵敏度和权衡分析,其几何形状(氢气流动角度,氢气和氧气流动面积以及氧气后尖端厚度)得到了优化,以达到理想的性能目标(燃烧长度) )和寿命/生存能力(氧化剂柱尖端和喷射器表面的最高温度以及燃烧室壁温)。使用几何均值方法进行了初步的多目标优化研究。此后,利用基于目标的替代模型和多目标最优模型的可用数据,进行基于方差的非参数方法和部分相关系数的敏感性分析,以确定设计变量对目标变异性的贡献。分析设计变量和目标的可变性;总而言之,本论文提供了一种用于Navier-Stokes计算的改进的从粗到细网格外推技术的见解,并为设计人员提供了针对给定设计问题进行设计优化研究和相关灵敏度分析的工具。

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