Ananalytical and Experimental Study of T - Shaped Composite Stiffened Panels: Effect of 90° Plies in Stringers on Curing and Buckling Performance
Author:
Publisher
Springer Science and Business Media LLC
Subject
Ceramics and Composites
Link
https://link.springer.com/content/pdf/10.1007/s10443-020-09816-4.pdf
Reference49 articles.
1. Anandan, S., Dhaliwal, G.S., Huo, Z., Chandrashekhara, K., Apetre, N., Iyyer, N.: Curing of thick thermoset composite laminates: multiphysics modeling and experiments [J]. Appl. Compos. Mater. 25(5), 1155–1168 (2018)
2. Taczała, M., Buczkowski, R., Kleiber, M.: Nonlinear buckling and post-buckling response of stiffened FGM plates in thermal environments [J]. Compos. Part B. 109, 238–247 (2017)
3. Anyfantis, K.N., Tsouvalis, N.G.: Post buckling progressive failure analysis of composite laminated stiffened panels [J]. Appl. Compos. Mater. 19(3–4), 219–236 (2012)
4. Yang, Z.Y., Zhang, J.B., Xie, Y.J., Zhang, B.M., Sun, B.G., Guo, H.J.: Influence of layup and curing on the surface accuracy in the manufacturing of carbon Fiber reinforced polymer (CFRP) composite space mirrors. Appl. Compos. Mater. 24, 1447–1458 (2017)
5. Hassan, M.H., Othman, A.R., Kamaruddin, S.: A review on the manufacturing defects of complex-shaped laminate in aircraft composite structures [J]. Int. J. Adv. Manuf. Technol. 91, 9–12 (2017)
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