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
Your Session has timed out. Please sign back in to continue.


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.


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



Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In