Abstract
In this chapter gradient and Hessian information computed using automatic differentiation and the adjoint method is applied to approximate Monte Carlo simulations for a geometric uncertainty analysis involving a sinusoidally pitching airfoil.
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Rumpfkeil, M.P., Yamazaki, W., Mavriplis, D.J. (2011). Uncertainty Analysis Utilizing Gradient and Hessian Information. In: Kuzmin, A. (eds) Computational Fluid Dynamics 2010. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-17884-9_32
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DOI: https://doi.org/10.1007/978-3-642-17884-9_32
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