Abstract
References 1 Sharifi, P. and Yates, D. N., Nonlinear Thermo-Elastic-Plastic and Creep Analysis by the Finite Element Method, AIAA Journal, Vol. 12, Sept. 1974, pp. 1210-1215. 2 Clough, R. W. and Felippa, C. A., A Refined Quadrilateral Element for Analysis of Plate Bending, Proceedings of Second Conference on Matrix Methods in Structural Mechanics, AFFDL-TR68-150, Oct. 1968, Air Force Flight Dynamics Lab., Wright-Patterson Air Force Base, Ohio, pp. 399-440. 3 Suarez, J. A., Composite Wing Structures, Stability Analysis of Advanced Filamentary Composite Panels, Tech. Rept. AC-SM-8087, May 1970, Grumman Aircraft Engineering Corp., Bethpage, N.Y. 4 Kaminski, B. E. and Ashton, J. E., Diagonal Tension Behavior of Boron-Epoxy Shear Panels, Journal of Composite Materials, Vol. 5, Oct. 1971, pp. 553-558. 5 Bushnell, D., Stress, Stability, and Vibration of Complex Branched Shells of Revolution: Analysis and User's Manual for BQSQR4, LMSC-D243605, March 1972, Lockheed Missiles & Space Co., Sunnyvale, Calif. Also CR 2116, Oct. 1972, NASA.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
