1. Minimization of thermal expansion of symmetric, balanced, angle ply laminates by optimization of fiber path configurations;Rangarajan;Compos Sci Technol,2011
2. Thermally-induced, geometrically nonlinear response of symmetrically laminated composite plates;Meyers;Compos Eng,1992
3. Optimal design of symmetrically laminated plates for maximum buckling temperature;Walker;J Therm Stresses,1997
4. Composite laminates with spatially varying fiber: variable stiffness panel concept;Gürdal,1992
5. Olmedo RA, Gürdal Z. Buckling response of laminates with spatially varying fiber orientations, AIAA/ASME/ASCE/AHS/ASC 34th structures, structural dynamics and materials conference, and AIAA/ASME adaptive structures Forum, La Jolla, CA, Apr. 19–22, 1993, Technical Papers. Pt. 4 (A93-33876 13–39), p. 2261–2269.