Axial Passive Damping Testing of Mass-Produced Stress Coupled, Cocured Damped Composites
Author:
Affiliation:
1. Boeing Phantom Works, Seattle, Washington 98124-2499
2. Brigham Young University, Provo, Utah 84602
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1974
Reference6 articles.
1. Enhanced damping of continuous wave fiber composite sandwich panels
2. Olcott, D. “Improved Damping in Composite Structures Through Stress Coupling, Co-Cured Damping Layers, and Segmented Stiffness Layers,” Ph.D. Dissertation,Dept. of Mechanical Engineering, Brigham YoungUniv., Provo, UT,1992.
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