Static Properties of Fibre Metal Laminates
Source abstract
Abstract
In this article a brief overview of the static properties of Fibre Metal Laminates is given. Starting with the stress-strain relation, an effective calculation tool for uniaxial stress-strain curves is given. The method is valid for all Glare types. The Norris failure model is described in combination with a Metal Volume Fraction approach leading to a useful tool to predict allowable blunt notch strength. The Volume Fraction approach is also useful in the case of the shear yield strength of Fibre Metal Laminates. With the use of the Iosipescu test shear yield properties are measured.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Structural Load-Bearing Analysis · Mechanical Behavior of Composites · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (11)
Show source-provided references
1. Gürdal, Z., Haftka, T. and Hajela, P., Design and Optimization of Laminated Composite Materials, Virginia Polytechnic Institute and State University, University of Florida, Rensselaer Polytechnic Institute, 1998.
2. Besseling, J. F. and van der Giessen, E., Mathematical Modelling of Inelastic Deformation, Engineering Mechanics & Continuum Mechanics and New Materials, Delft University of Technology, Delft, The Netherlands, 1993.
3. van Rijn, J. C. F. N., ‘A Calculation Method for the Stress-Strain Curves of Glare 3 and Glare 4B,’ National Aerospace Laboratory, Report NLR-CR-2000-172 (restricted), Amsterdam, April 2000.
4. Sun, C. T. et al., Comparative Evaluation of Failure Analysis Methods for Composite Laminates, U.S. Department of transportation, Federal Aviation Administration, Washington, D.C., 1996.
5. Roebroeks, G., ‘The Metal Volume Fraction Approach,’ TD-R-00-003, Structural Laminates Industries, Delft, 2000.
6. Bosker, O. J., ‘Glare Uni-Axial Blunt Notch Test Results,’ B2V-99-27, Delft University of Technology, Delft, 2000.
7. Wu, H. F., Slagter, W. J. and Verolme, J. L., ‘A Pilot Study of Metal Fraction Approach for Fiber Metal Laminates,’ Product Design and Mechanical Division, Alcoa Technical Center, U.S.A., Faculty of Aerospace Engineering, Delft University of Technology, The Netherlands, ATC Report No. 57-92-17, SLC Report No. SL-020-B, December 1992.
8. Mattousch, A. C., ‘Shear Properties of Glare 3-3/2-0.2 and Glare 3-3/2-0.3,’ SLI Report TD-R-95-001, 7 March 1995.
9. Kuijpers, P. K., ‘The Influence of Material Changes on the Shear Strength of Glare 3 Laminates,’ Report B2v-98-30, Delft University of Technology, November 1998.
10. Kuijpers, P. L., ‘Results of Shear Tests,’ Report B2v-99-36, Delft University of Technology, October 1999.
11. Hagenbeek, M., ‘The MVF Method for Shear Yield Strength Prediction,’ Report B2v-99-26, Delft University of Technology, October 1999.