An Updating Method of Aero Tyre Model by Shimmy Test
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-8861-7_54
Reference33 articles.
1. Sanches, L., Guimarães, T.A., Marques, F.D.: Nonlinear energy sink to enhance the landing gear shimmy performance. Acta Mech. 232(7), 2605–2622 (2021)
2. Thota, P., Krauskopf, B., Lowenberg, M.: Interaction of torsion and lateral bending in aircraft nose landing gear shimmy. Nonlinear Dyn. 57(3), 455–467 (2009)
3. Rahmani, M., Behdinan, K.: Interaction of torque link freeplay and Coulomb friction nonlinearities in nose landing gear shimmy scenarios. Int. J. Non-Linear Mech. 119, 103338 (2020)
4. Feng, F., Nie, H., Zhang, M., et al.: Effect of torsional damping on aircraft nose landing-gear shimmy. J. Aircr. 52(2), 561–568 (2015)
5. Howcroft, C., Krauskopf, B., Lowenberg, M.H., et al.: Influence of variable side-stay geometry on the shimmy dynamics of an aircraft dual-wheel main landing gear. J. Appl. Dyn. Syst. 12(3), 1181–1209 (2013)
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