Time-Varying Objective Functions for Optimum Shape Design via Control Theory-Reference-Cited by-同舟云学术

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Time-Varying Objective Functions for Optimum Shape Design via Control Theory

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Tatossian Charles¹,Nadarajah Siva¹

Affiliation:

1. McGill University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1274

Reference15 articles.

1. Computational Aerodynamics for Aircraft Design

2. Optimum aerodynamic design using CFD and control theory

3. Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow

4. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers

5. Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation

Cited by 3 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. Rotor Airfoil Design Optimization Based on Unsteady Flow;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2017

2. A NLFD Method for the Simulation of Periodic Unsteady Flows for Overset Meshes;19th AIAA Computational Fluid Dynamics;2009-06-14

3. Optimum Shape Design of Helicopter Rotors via Control Theory;18th AIAA Computational Fluid Dynamics Conference;2007-06-15

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