1. Liu, J., Zhang, S., and Wang, Z., “Experiment and Simulation on the Incremental Bend Forming Technology of the Integral Wing-Skin Panel,” Metal Forming Technology, Vol. 21, No. 6, pp. 23–25, 2003. (in Chinese)
2. Yan, Y., Wan, M., and Wang, H.-B., “FEM Equivalent Model for Press Bend Forming of Aircraft Integral Panel,” Transactions of Nonferrous Metals Society of China, Vol. 19, No. 2, pp. 414–421, 2009.
3. Dong, Y., “Prediction and Control of Fracture in Multi-Point Press Forming of Aluminum Alloy Integral Panel,” Jilin University, 2016. (In Chinese)
4. Lei, X., Tan, J., Zhan, M., and Gao, P., “Dependence of Electromagnetic Force on Rib Geometry in the Electromagnetic Forming of Stiffened Panels,” The International Journal of Advanced Manufacturing Technology, Vol. 94, Nos. 1-4, pp. 217–226, 2018.
5. Lam, A. C., Shi, Z., Yang, H., Wan, L., Davies, C. M., et al., “Creep-Age Forming AA2219 Plates with Different Stiffener Designs and Pre-Form Age Conditions: Experimental and Finite Element Studies,” Journal of Materials Processing Technology, Vol. 219, pp. 155–163, 2015.