Shape Optimization of Rectangular Plates for Vibration-Based Fatigue Testing
Author:
Affiliation:
1. Mechanical and Aerospace Engineering, Utah State University, 4130 Old Main Hill, Logan, UT 84322
2. Air Force Research Laboratory, Aerospace Systems Directorate, Bldg 18D, Wright-Patterson AFB, Dayton, OH 45433
Abstract
Funder
Air Force Office of Scientific Research
Air Force Research Laboratory
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/88/9/091001/6690054/jam_88_9_091001.pdf
Reference31 articles.
1. Fatigue of Materials
2. A Critical Analysis of Crack Propagation Laws;Paris;ASME J. Basic Eng.,1963
3. A Review of Critical Plane Orientations in Multiaxial Fatigue Failure Criteria of Metallic Materials;Karolczuk;Int. J. Fract.,2005
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