Adjoint-based Shape Optimization of High-lift Airfoil using the NSU2D Unstructured Mesh Solver-Reference-Cited by-同舟云学术

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Adjoint-based Shape Optimization of High-lift Airfoil using the NSU2D Unstructured Mesh Solver

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Nambu Taisuke¹,Mavriplis Dimitri J.²,Mani Karthik²

Affiliation:

1. Waseda University

2. University of Wyoming, Laramie

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0554

Reference30 articles.

1. Jameson, A., Alonso, J. J., Reuther, J. J., Martinelli, L. and Vassberg, J. C. "Aerodynamic shape optimization techniques based on control theory" AIAA Paper 98-2538.

2. Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes

3. Practical Three-Dimensional Aerodynamic Design and Optimization Using Unstructured Meshes

Cited by 7 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. Optimization of High-Lift Systems at Takeoff Conditions Subject to Kinematic Constraints;Journal of Aircraft;2022-07

2. Singlepoint and Multipoint Robust Design of Airfoils using CST Functions;AIAA Scitech 2021 Forum;2021-01-04

3. New Family of Airfoils for the Conceptual Design of Aircraft with Variable-Camber Wings;AIAA Aviation 2019 Forum;2019-06-14

4. Nonconsistent Mesh Movement and Sensitivity Calculation on Adjoint Aerodynamic Optimization;AIAA Journal;2018-04

5. A Hybrid Dynamic Mesh Generation Method for Multi-Block Structured Grid;Advances in Applied Mathematics and Mechanics;2017-01-18

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