Structural tailoring of aircraft engine blade subject to ice impact constraints
Author:
Affiliation:
1. Sverdrup Technology, Inc., Brook Park, OH
2. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4710
Reference8 articles.
1. An efficient feasible directions algorithm for design synthesis
2. Reduction of stiffness and mass matrices
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