Abstract
Gurdal, Z., and Olmedo, R., In-Plane Response of Laminates with Spatially Varying Fiber Orientations: 'Variable Stiffness Panel Concept', AIAA Journal, Vol. 31, No. 4, 1993, pp. 751-758. Biggers, S. B., and Srinivasan, S., Buckling Response of Tailored Rectangular Composite Plates, AIAA Journal, Vol. 31, No. 3, 1993, pp. 590-596. Biggers, S. B., and Srinivasan, S., Improved Compression Buckling for Rectangular Composite Plates by Stiffness Tailoring, Enhancing Analysis Techniques for Composite Materials, NDE Vol. 10, ASME, New York, 1991, pp. 187-195. HKS (Hibbitt, Karlsson, and Sorensen), Inc., ABAQUS Theory and User's Manuals, Version 4.8, HKS, Pawtucket, RI, 1989, pp. 2.2.7-1, 3.4.3-13.4.3-6. Dow, M. B., and Smith, D. L., Properties of Two Composite Materials Made of Toughened Epoxy Resin and High-Strain Graphite Fiber, NASA TP-2826, 1988. only dynamic ones in that of the mass matrix. The present algorithm is confined for framed structures (truss and beam members), and does not address the issue of noise, as it is based on real test data (which are assumed to be accurate).
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