Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design-Reference-Cited by-同舟云学术

Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Nielsen Eric¹,Park Michael¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-491

Reference48 articles.

1. Wing Design by Numerical Optimization

2. DESIGN OPTIMIZATION OF TRANSONIC AIRFOILS

3. Vanderplaats, G.N., Hicks, R.N., and Murman, E.M. "Application of Numerical Optimization Techniques to Airfoil Design," NASAConferenceonAerodynamicAnalysisRequiringAdvancedComputers,"NASASP-347,PartII,March1975.

4. Aerodynamic Sensitivity Analysis Methods for the Compressible Euler Equations

5. Borggaard, J.T., Burns, J., Cliff, E.M., and Gunzburger, M.D. "Sensitivity Calculations for a 2-D Inviscid Supersonic ForebodyProblem,"IdentificationandControlSystemsGovernedbyPartialDifferentialEquations,SIAMPublications,Philadelphia,1993,pp.14-24.

Cited by 14 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. Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction;54th AIAA Aerospace Sciences Meeting;2016-01-02

2. Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings;53rd AIAA Aerospace Sciences Meeting;2015-01-03

3. Applications of a discrete viscous adjoint method for aerodynamic shape optimisation of 3D configurations;CEAS Aeronautical Journal;2011-10-28

4. Aerodynamic Optimization Algorithm with Integrated Geometry Parameterization and Mesh Movement;AIAA Journal;2010-02

5. Aerodynamic Shape Optimization Using First and Second Order Adjoint and Direct Approaches;Archives of Computational Methods in Engineering;2008-08-14