Three-dimensional aerodynamic shape sensitivity analysis and design optimization using the Euler equations on unstructured grids-Reference-Cited by-同舟云学术

Three-dimensional aerodynamic shape sensitivity analysis and design optimization using the Euler equations on unstructured grids

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:14th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Newman, III James¹,Taylor, III Arthur¹

Affiliation:

1. Old Dominion Univ., Norfolk, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2464

Reference34 articles.

1. Aerodynamic design via control theory

2. Eleshaky, M.E., and Baysal, O. "Shape Optimization of a 3D Nacelle Near a Flat Plate Wing Using Multiblock Sensitivity Analysis,'' AIAA Paper 94-0160,Jan. 1994.

3. Taylor, A.C. 111, "AutomaticDifferentiationof Advanced Flow-Analysis Codcs in Incremciital Iterative Form for Multidisciplinary Applications,"Final Report, Master Contract NAS1-19858 (Task No. 77),Nov. 1995.

Cited by 16 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. Parallel Implementation of Localized Radial Basis Function Interpolation for Computational Aeroelastic Predictions;Communications in Computer and Information Science;2014

2. Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches;Computers & Fluids;2010-03

3. Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design;AIAA Journal;2006-05

4. Efficient Construction of Discrete Adjoint Operators on Unstructured Grids Using Complex Variables;AIAA Journal;2006-04

5. Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10