1. Gavva LM, Endogur AI (2018) Statics and buckling problems of aircraft structurally- anisotropic composite panels with the influence of production technology. IOP Conf Ser 312(1):012009
2. Andrienko VM, Belous VA (2001) Optimal design of wing box composite panels with strength and buckling restrictions. TSAGI Proc 2642:151–158
3. Mitrophanov OV (1998) Estimation of some approaches to composite wing weight decreasing and optimal reinforcement of stiffened panels with buckling restrictions. Air fleet equipment V 72(1):36–40
4. Mitrophanov OV, Strelyaev DV (1999) Optimal design of composite stiffened panels of aerospace aircraft Shuttle. MGTU CA Science Proc 13:31–34
5. Yoko K, Kameyama M, Ning H, Fukunaga H (2004) Optimum design of composite wing considering stiffened panel buckling. Nihon kikai ronbunshu A V 70(691):479–486