Multi-objective Vibro-acoustic Optimization of Stiffened Panels Excited by Acoustic Diffuse Field
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1750
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1. BOUNDARY LAYER INDUCED NOISE IN AIRCRAFT, PART I: THE FLAT PLATE MODEL
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2. Multi-objective Optimization of Non-uniform Beam for Minimum Weight and Sound Radiation;Transactions of Tianjin University;2017-05-19
3. Experimental Validation of the EBF3PanelOpt Vibroacoustic Analysis of Stiffened Panels;Journal of Aircraft;2015-09
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