Load and Response Prediction Using Numerical Methods in Acoustic Fatigue
Author:
Affiliation:
1. Division of Structural Mechanics, Lund University, SE-221 00 Lund, Sweden
2. Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati, Ohio 45221-0070
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033414
Reference25 articles.
1. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
2. ClarksonB. “Review of Sonic Fatigue Technology,” NASA TR-CP-4587, 1994.
3. Dynamic response of doubly curved honeycomb sandwich panels to random acoustic excitation. Part 1: Experimental study
4. Dynamic response of doubly curved honeycomb sandwich panels to random acoustic excitation. Part 2: Theoretical study
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