CAD and CAE integration with application to the forging shape optimization of turbine disks
Author:
Affiliation:
1. GE Corporate R & D Center, Schenectady, NY
2. GE Power Systems, Schenectady, NY
3. GE Aircraft Engines, Cincinnati, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2032
Reference17 articles.
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. Aerodynamic Design of Wing-Body-Nacelle-Pylon Configuration;17th AIAA Computational Fluid Dynamics Conference;2005-06-06
2. A practical approach to forging optimization;8th Symposium on Multidisciplinary Analysis and Optimization;2000-09-06
3. A federated intelligent product environment;8th Symposium on Multidisciplinary Analysis and Optimization;2000-09-06
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