Rapid convergence of airfoil design problems using progressive optimization

Author:

Dadone A.,Grossman B.

Publisher

Springer Berlin Heidelberg

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A general use adjoint formulation for compressible and incompressible inviscid fluid dynamic optimization;Computers & Fluids;2019-01

2. A General Purpose Adjoint Formulation for Inviscid 2D/3D Fluid Dynamic Optimization;10th AIAA Multidisciplinary Design Optimization Conference;2014-01-10

3. A General Purpose Discrete Adjoint Formulation for Inviscid Flow Nozzle Design;49th AIAA/ASME/SAE/ASEE Joint PropulsionConference;2013-07-12

4. A General Purpose Discrete Adjoint Formulation for Inviscid Two-Dimensional Fluid Dynamic Optimization;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

5. Fast Convergence of Viscous Airfoil Design Problems;AIAA Journal;2002-10

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