Abstract
In this article, we apply a new airfoil shape optimization algorithm based on adaptive higher order Discontinuous Galerkin methods with discretization error control to a 2D benchmark problem of the AIAA Design Optimization Discussion Group. Each flow solution in the optimization process is computed on a sequence of goal-oriented h- or hp-refined meshes until the estimation of the discretization error in a given target quantity (like the drag coefficient) is below a prescribed error tolerance. Furthermore, the optimization is driven by the Sequential Quadratic Programming (SQP) algorithm and the corresponding gradient of the objective function is evaluated via the adjoint approach. Finally, the effect of the discretization error on the quality of the optimized airfoil shapes is investigated.
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References
Becker, R., Rannacher, R.: An optimal control approach to a posteriori error estimation in finite element methods. Acta Numerica 10, 1–102 (2001)
Caglar, H., Akansu, A.N.: A generalized parametric PR-QMF design technique based on Bernstein polynomial approximation. IEEE Trans. Sig. Process. 41(7), 2314–2321 (1993)
Carrier, G., Destarac, D., et al.: Gradient-based aerodynamic optimization with the elsA software. In: 52nd AIAA Aerospace Sciences Meeting, SciTech, 2014, AIAA-2014-0568 (2014)
Hartmann, R.: Adjoint consistency analysis of discontinuous Galerkin discretizations. SIAM J. Numer. Anal. 45(6), 2671–2696 (2007)
Hartmann, R., Held, J., Leicht, T., Prill, F.: Discontinuous Galerkin methods for computational aerodynamics-3D adaptive flow simulation with the DLR PADGE code. Aerosp. Sci. Technol. 14, 512–519 (2010)
Hartmann, R., Houston, P.: Adaptive discontinuous Galerkin finite element methods for the compressible Euler equations. J. Comput. Phys. 183(2), 508–532 (2002)
Hicks, R.M., Henne, P.: Wing design by numerical optimization. J. Aircr. 15, 407–412 (1978)
https://info.aiaa.org/tac/ASG/APATC/AeroDesignOpt-DG/default.aspx
Jameson, A.: Optimum aerodynamic design using CFD and control theory. In: 12th Computational Fluid Dynamics Conference, AIAA Paper 95–1729 (1995)
Leicht, T., Hartmann, R.: Error estimation and hp-adaptive mesh refinement for discontinuous Galerkin methods. In: Wang, ZJ. (ed.) Adaptive High-Order Methods in Computational Fluid Dynamics, Advances in Computational Fluid Dynamics, vol. 2, Chap. 3, pp. 67–94. World Science Books (2011)
Li, D., Hartmann, R.: Adjoint-based airfoil optimization with discretization error control. Int. J. Numer. Meth. Fluids 77(1), 1–17 (2015)
Lu, J.: An a posteriori error control framework for adaptive precision optimization using discontinuous Galerkin finite element method. PhD thesis, M.I.T. (2005)
Mavriplis, C.: Adaptive mesh strategies for the spectral element method. Comput. Methods Appl. Mech. Engrg. 116, 77–86 (1994)
Nocedal, J., Wright, SJ.: Numerical Optimization. Springer (2006)
Vassberg, J.C., Harrison, N., Roman, D., Jameson, A.: A systematic study on the impact of dimensionality for a two-dimensional aerodynamics optimization model problem. In: 29th AIAA Applied Aerodynamic Conference, AIAA 2011–3176 (2011)
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Li, D., Hartmann, R. (2016). Adjoint-Based Error Estimation and Mesh Refinement in an Adjoint-Based Airfoil Shape Optimization of a Transonic Benchmark Problem. In: Dillmann, A., Heller, G., Krämer, E., Wagner, C., Breitsamter, C. (eds) New Results in Numerical and Experimental Fluid Mechanics X. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 132. Springer, Cham. https://doi.org/10.1007/978-3-319-27279-5_47
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DOI: https://doi.org/10.1007/978-3-319-27279-5_47
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