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- W90508489 abstract "An efficient multi-block Newton‐Krylov algorithm using the compressible Navier‐Stokes equations is presented for the analysis and design of high-lift airfoil configurations. The preconditioned generalized minimum residual (GMRES) method is applied to solve the discreteadjoint equation, leading to a fast computation of accurate objective function gradients. Furthermore, the GMRES method is used in conjunction with an inexact-Newton approach to obtain fast solutions of the Navier‐Stokes equations. Optimization constraints are enforced through a penalty formulation, and the resulting unconstrained problem is solved via a quasi-Newton method. Several design examples are provided which demonstrate that this algorithm provides an effective and practical tool for the design of multi-element airfoil configurations." @default.
- W90508489 created "2016-06-24" @default.
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- W90508489 date "2002-01-01" @default.
- W90508489 modified "2023-09-26" @default.
- W90508489 title "FROM ANALYSIS TO DESIGN OF HIGH-LIFT CONFIGURATIONS USING A NEWTON-KRYLOV ALGORITHM" @default.
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