2010
DOI: 10.14495/jsiaml.2.37
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Numerical solution to shape optimization problems for non-stationary Navier-Stokes problems

Abstract: The present paper describes a numerical solution of shape optimization problems for nonstationary Navier-Stokes problems. As a concrete example, we consider the problem of finding the shape of an obstacle in a flow field in order to minimize the energy loss integral for an assigned time interval. The primary goal of the present paper is to demonstrate the evaluation of the shape derivative of the energy loss. The traction method is used for the reshaping algorithm. Numerical results show that the shapes of the… Show more

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Cited by 8 publications
(3 citation statements)
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References 13 publications
(15 reference statements)
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“…Subsequently, J. Haslinger and R. A. Makinen [4], B. Mohammadi and O. Pironneau [5], and M. Moubachir and J. P. Zolesio [6] constructed fundamental frameworks of flow-field shape-optimization problems. Recently, many researchers are examining the topic [7][8][9][10]. Efficient but accurate numerical methods must be used for such flow computations within an optimization process.…”
Section: Introductionmentioning
confidence: 99%
“…Subsequently, J. Haslinger and R. A. Makinen [4], B. Mohammadi and O. Pironneau [5], and M. Moubachir and J. P. Zolesio [6] constructed fundamental frameworks of flow-field shape-optimization problems. Recently, many researchers are examining the topic [7][8][9][10]. Efficient but accurate numerical methods must be used for such flow computations within an optimization process.…”
Section: Introductionmentioning
confidence: 99%
“…In 1973, Pironneau [1] pioneered a structural optimization method for fluid dynamics problems, and obtained minimum drag wing profiles under Stokes flow. Considerable research has been carried out since then and a number of structural optimization methods applicable to fluid dynamics problems have been proposed [2][3][4][5][6][7][8][9][10][11]. However, since the above research was based on shape optimization, the feasible design modifications only consisted in the adjustment of the boundaries of selected parts to the fluid domain.…”
Section: Introductionmentioning
confidence: 99%
“…The remaining boundaries of the channel are wall boundaries denoted by Γ w , upon which -together with the obstacle boundary Γ f -a no-slip boundary condition is imposed on the fluid. We refer the reader to [11,15,21,25,33] for shape optimization problems involving fluids among others. We also point out that usually, the curl ∇ × u is enough to quantify the vorticity of the fluid.…”
mentioning
confidence: 99%