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TECHNICAL PAPERS

Experimental Investigation of Residual Stresses in Layered Materials Using Moiré Interferometry

[+] Author and Article Information
Keith B. Bowman, David H. Mollenhauer

Air Force Research Laboratory, Materials and Manufacturing Directorate, Wright-Patterson Air Force Base, OH 45433-7750

J. Electron. Packag 124(4), 340-344 (Dec 12, 2002) (5 pages) doi:10.1115/1.1497627 History: Received May 01, 2002; Online December 12, 2002
Copyright © 2002 by ASME
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References

Puppo,  A. H., and Evensen,  H. A., 1970, “Interlaminar Shear in Laminated Composites Under Generalized Plane Stress,” J. Compos. Mater., 4, pp. 204–212.
Pipes,  R. B., and Pagano,  N. J., 1970, “Interlaminar Stresses in Composite Laminates Under Uniform Axial Extension,” J. Compos. Mater., 4, pp. 538–548.
Wang,  A. S. D., and Crossman,  F. W., 1977, “Edge Effects on Thermally Induced Stresses in Composite Laminates,” J. Compos. Mater., 11, pp. 300–312.
Treuting,  R. G., and Read,  W. T., 1951, “A Mechanical Determination of Biaxial Residual Stress in Sheet Materials,” J. Appl. Phys., 22, pp. 130–134.
SAE J936, 1965, “Methods of Residual Stress Measurement,” Handbook Supplement J936, Society of Automotive Engineers.
Greving,  D. J., Rybicki,  E. F., and Shadley,  J. R., 1994, “Through-Thickness Residual Stress Evaluations for Several Industrial Thermal Spray Coatings Using Modified Layer-Removal Method,” Journal of Thermal Spray Technology, 3(4), pp. 379–388.
Post, D., “Moiré Interferometry, 1987,” Handbook of Experimental Mechanics, Chapter 7, A. S. Kobayashi, ed., Prentice-Hall, Englewood Cliff, NJ.
3M Scotch-Weld Technical Data, 1999, “Structural Film Adhesive AF-191,” 3M Corporation, St. Paul MN, Issue No. 4.
Iarve,  E. V., 1996, “Spline Variational Three Dimensional Stress Analysis of Laminated Composite Plates with Open Holes,” Int. J. Solids Struct., 33(14), pp. 2095–2118.
Mollenhauer,  D., Ifju,  P., and Han,  B., 1994, “A Compact, Robust, and Versatile Moiré Interferometer,” Optics and Lasers in Engineering, 22, pp. 29–40.

Figures

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Schematic of the MRFEE method specimen (a) Full specimen with diffraction grating on front edge; (b) after the initial cut; and (c) the removal of the layers of the top material
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Comparison of the MLRM and BSAM strain values for the samples with polymer thicknesses of (a) 3.57 mm and (b) 1.66 mm
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Comparison of the MLRM and BSAM stress results for the samples with polymer thicknesses of (a) 3.57 mm and (b) 1.66 mm
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The 5.08-cm×2.54-cm specimen configuration (a) with diffraction grating, (b) after sectioning cut, and (c) with layers removed after milling
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Milling setup with sample and cutter
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Displacement contours on the polymer free edge in the (a) horizontal and (b) vertical fields

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