Reduction of the Adjoint Gradient Formula in the Continuous Limit

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Optimization and Computational Fluid Dynamics (2008, methodology): “, in control problems were developed in [31, 32].”
Direct, adjoint and mixed approaches for the computation of Hessian in airfoil design problems (2008, unknown): “Among them, it is appropriate to mention the one-shot algorithm, in which the flow (state), adjoint (costate) and optimization equations are solved simultaneously [14, 15], the incomplete gradient method that skips the computation of costly terms [16], the reduced gradient method that overcomes grid”