Journal
AIAA JOURNAL
Volume 47, Issue 1, Pages 271-282Publisher
AMER INST AERONAUT ASTRONAUT
DOI: 10.2514/1.40291
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Funding
- Francois-Xavier Bagnoud (FXB)
- Center for Rotary and Fixed Wing Air Vehicle Design
- NASA [NNA-06CB71H]
- Institute for Future Space Transport
- National Science Foundation [0423280]
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The advantages of using multiple surrogates for approximation and reduction of helicopter vibration are studied. Multiple approximation methods, including a weighted-average approach, are considered so that pitfalls associated with only using a single best surrogate for. the rotor blade vibration-reduction problem are avoided. A vibration objective function corresponding to a flight condition in which blade-vortex interaction causes high levels of vibration is considered. The design variables consist of cross-sectional dimensions of the structural member of the blade and nonstructural masses. The optimized designs are compared with a baseline design resembling a Messerschmitt-Bolkow-Blohm BO-105 blade. The results indicate that at relatively little additional cost compared with optimizing a single surrogate, multiple surrogates can be used to locate various reduced-vibration designs that would be overlooked if only a single approximation method was employed, and the most accurate surrogate may not lead to the best design.
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