Author:
Xu Bo,Zhao Chaoze,Gong Bo,An Chunyu,Wen Xiaodong
Publisher
Springer Nature Switzerland
Reference14 articles.
1. Fu, Y., Fu, H., Zhang, S.: A novel safe life extension method for aircraft main landing gear based on statistical inference of test life data and outfield life data. Symmetry 15(4), 880 (2023)
2. Voevodin, A.V., Kornyakov, A.A., Petrov, A.S., Petrov, D.A., Sudakov, G.G.: Improvement of the take-off and landing characteristics of wing using an ejector pump. Thermophys. Aeromech. 26, 9–18 (2019)
3. Aftab, S.G., Sreedhara, B., Ganesh, E., Babu, N.R., Aithal, S.K.: Finite element analysis of a passenger aircraft landing gear for structural and fatigue safety. Mater. Today: Proc. 54, 152–158 (2022)
4. Bagnoli, F., Dolce, F., Colavita, M., Bernabei, M.: Fatigue fracture of a main landing gear swinging lever in a civil aircraft. Eng. Fail. Anal. 15(6), 755–765 (2008)
5. Xue, C.J., Dai, J.H., Wei, T., Liu, B., Deng, Y.Q., Ma, J.: Structural optimization of a nose landing gear considering its fatigue life. J. Aircr. 49(1), 225–236 (2012)