Shape sensitivity analysis for the work functional

P. Plotnikov, J. Sokołowski
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Abstract

The non stationary, compressible Navier-Stokes equations are considered in a bounded hold-all domain. The nonhomegeneous boundary conditions are prescribed on the boundary of hold-all domain. The existence of the so-called weak normalized solutions for the model is established in [2]. In this talk we consider the associated shape optimization problems for the model. In the stationary case the drag of an obstacle is minimized. In the non stationary case the work for a fight scenario of an obstacle is minimized. It means that the boundary of an obstacle flying in a gas is optimized in such a way that for the given trajectory the energy required to attain a given point in the domain is minimized with respect to the shape of the obstacle. The family of admissible obstacles is sufficiently general and includes the standard shapes of an airfoil. We present the new results on the shape sensitivity analysis of the work functional for non stationary compressible Navier-Stokes equations [1]. In particular, the shape gradient is determined for the shape functional. The obtained results can be justified from mathematical point of view for the local solutions, or the global classical solutions of the model.
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工作函式的形状灵敏度分析
研究非平稳、可压缩的Navier-Stokes方程在有界保持全域上的性质。在hold-all域的边界上规定了非齐次边界条件。该模型的所谓弱归一化解的存在性在[2]中得到了证明。在这次演讲中,我们考虑了模型的相关形状优化问题。在静止情况下,障碍物的阻力最小。在非静止情况下,对于障碍物的战斗场景的功被最小化。这意味着在气体中飞行的障碍物的边界以这样一种方式进行优化,即对于给定的轨迹,相对于障碍物的形状,在区域内达到给定点所需的能量最小。可接受的障碍的家庭是足够普遍的,包括一个翼型的标准形状。我们提出了非平稳可压缩Navier-Stokes方程的功泛函的形状敏感性分析的新结果[1]。特别地,形状梯度是为形状函数确定的。所得结果可以从数学角度对模型的局部解或全局经典解进行证明。
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