Author:
Nitin Chandola ,Rawat Rohit Singh
Reference12 articles.
1. Jweeg, M.J., Abid-Aun, S.H.: Optimization of Light Weight Aircraft Wing Structure. Journal of Engineering & Development, Vol. 12, No. 1, March (2008).
2. Vinson, J.R.: Optimum Design of Composite Honeycomb Sandwich Panels Subjected to Uniaxial Compression. University of Delaware, AIAA Journal, Vol. 24, No. 10, October 1986, p. 1690–1696.
3. Iyengar, N.G.R., Joshi, S.P.: Optimal Design of Antisymmetric Laminated Composite Plates. Journal of Aircraft, Vol. 23, No. 5, May 1986, pp. 359–360.
4. Guo, S.J., Banerjee, J.R., Cheung, C.W.: The effect of laminate lay-up on the flutter speed of composite wings. Proceedings of the Institution of Mechanical Engineers, Part G: journal of aerospace engineering, Vol. 217, No. 3, 2003, pp. 115–122.
5. Belega, B.A.: Bird-strike impact simulation with an aircraft wing using SPH bird model. INCAS Bulletin. Vol. 7 Issue 3, pp. 51–58, 2015.