Publisher
American Institute of Aeronautics and Astronautics
Cited by
2 articles.
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1. Development of multidisciplinary optimization procedure for gas turbine blade design;37th Aerospace Sciences Meeting and Exhibit;1999-01-11
2. Multidisciplinary optimization of gas turbine blade design;7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;1998-08-22