Technique for Developing Design Tools from the Analysis Methods of Computational Aerodynamics

Author:

Davis Warren H.1

Affiliation:

1. Grumman Aerospace Corp., Bethpage, N. Y.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

Cited by 11 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 Naturally Bounded Parameterization Method for Airfoil Shape Optimization;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04

2. Airfoil Shape Design and Optimization Using Multifidelity Analysis and Embedded Inverse Design;AIAA Journal;2006-09

3. Application of Inverse Design Method to Estimation of Wind Tunnel Models;Inverse Problems in Engineering Mechanics IV;2003

4. New Three-Dimensional Inverse Method for High-Speed Vehicle Design;Journal of Spacecraft and Rockets;1998-07

5. An inverse method for the design of transonic airfoils and wings;Inverse Problems in Engineering;1996-11

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