Decomposition-based optimization procedure for high-speed prop-rotors using composite tailoring
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287-6106
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference25 articles.
1. Selected design issues of some high speed rotorcraft concepts
2. DESIGN OF HIGH SPEED PROPROTORS USING MULTIOBJECTIVE OPTIMIZATION TECHNIQUES
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