Hostname: page-component-78c5997874-8bhkd Total loading time: 0 Render date: 2024-11-11T01:25:46.676Z Has data issue: false hasContentIssue false
  • English
  • Français

Numerical and experimental testing of aircraft tyre impact during landing

Published online by Cambridge University Press:  07 July 2021

Y. Gan Open the ORCID record for Y. Gan [Opens in a new window] ,
X. Fang ,
X. Wei  and
H. Nie
Y. Gan
Affiliation:
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics Nanjing Jiangsu, 210016China
X. Fang
Affiliation:
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics Nanjing Jiangsu, 210016China
X. Wei*
Affiliation:
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics Nanjing Jiangsu, 210016China State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing Jiangsu, 210016China
H. Nie
Affiliation:
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics Nanjing Jiangsu, 210016China State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing Jiangsu, 210016China
*
wei_xiaohui@nuaa.edu.cn
Get access Rights & Permissions [Opens in a new window]

Abstract

The capability of aircraft tyres to sustain landing impact loads is essential for flight landing safety. Hence, the development of a reliable experimental database is necessary to validate numerical models. The experimental data on aircraft tyre landing impact in the public literature are somewhat sparse. This paper describes a detailed design rig for aircraft tyre impact testing. A finite element model is then created and simulated using a finite element tool (ABAQUS). Inflation and static load simulations are analysed based on the FE tyre model to confirm its reliability. Comparison of experimental measurements with the results reveals that the model can predict the significant features of aircraft tyre impact in a landing scenario. Very little experimental data are publicly available to verify aircraft tyre models. Therefore, the experimental data in this paper fill this gap in the literature.

Keywords

Aircraft tyre impactFEALanding impact experiments
Type
Research Article
Information
The Aeronautical Journal , Volume 125 , Issue 1294 , December 2021 , pp. 2200 - 2216
Copyright
© The Author(s), 2021. Published by Cambridge University Press on behalf of Royal Aeronautical Society

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Kuruppu, K.D.D. and Hettiarachchi, C.J. Case study on aircraft tyre wear in Y12 aircraft tyres. Aeronaut. J., 2018, 122, pp 1123–1144.CrossRefGoogle Scholar
Kilner, J.R. Pneumatic tire model for aircraft simulation. J. Aircr., 1982, 19, pp 851–857.CrossRefGoogle Scholar
Anson, R., Pena, J. and Postic, R. Finite element analysis applied to radial aircraft tyre engineering. Proc. Inst. Nech. Eng. G, 1996, 210, pp 109–116.CrossRefGoogle Scholar
Behroozi, M., Olatunbosun, O.A. and Ding, W. Finite element analysis of aircraft tyre – effect of model complexity on tyre performance characteristics. Mater. Des., 2012, 35, pp 810–819.CrossRefGoogle Scholar
Reid, J.D., Boesch, D., Bielenber, R.W. Detailed tyre modelling for crash applications. Int J. Crashworthiness, 2007, 12, pp 521–529.CrossRefGoogle Scholar
Guo, H., Bastien, C., Blundell, M. and Wood, G. Development of a detailed aircraft tyre finite element model for safety assessment, Mater. Des., 2014, 53, pp 902–909.CrossRefGoogle Scholar
Baranowski, P., Malachowski, J., Janiszewski, J. and Wekezer, J., Detailed tyre FE modeling with multistage validation for dynamic analysis, Mater. Des., 2016, 35, 810–819.Google Scholar
Yao, S., Yue, Z., Geng, X. and Wang, P. Finite element analysis of aircraft tire for safety assessment with CV and CPM methods, Multidisc. Model. Mater. Struct., 2017, 13, pp 501–508.CrossRefGoogle Scholar
Essienubong, I.A., Ikechukwu, O.and Paul, S. Finite element analysis of aircraft tire behaviour under overloaded aircraft landing phase. Aeron Aero Open Access J., 2018, 2, pp 32–37.Google Scholar
Zhang, X., Xu, F., Ren, X., Gao, X. and Cao, R. Consideration on aircraft tire spray when running on wet runways, Chin. J. Aeronaut., 2020, 33, pp 520–528.CrossRefGoogle Scholar
Xia, Y., Yong, X. and Li, W. Study on the compressible hyperelastic constitutive model of tire rubber compounds under moderate finite deformation, Rubber Chem. Technol., 2004, 77, pp 230–241.CrossRefGoogle Scholar
Tanner, J.A., Daugherty, R.H. and Smith, H.C. Mechanical Properties of Radial-ply Aircraft Tires. SAE 2005-01-3438, USA: SAE International, 2005.Google Scholar
Ojala, J.K. Using ABAQUS in tire development process. In: ABAQUS users’ conference 2005, Pawtucket, USA; October 14, 2004.Google Scholar
Smith, L.P. The Language of Rubber: An Introduction to the Specification and Testing of Elastomers, Butterworth-Heinemann Ltd., 1993, London, p 257.Google Scholar
Chagno, G., Marckmann, G. and Verron, E. A comparison of the Hart-Smith model with Arruda-Boyce and gent formulations for rubber elasticity, Rubber Chem. Technol., 2004, 77, pp 724–735.CrossRefGoogle Scholar
Ali, A., Hosseini, M. and Sahari, B.B. A review of constitutive models for rubber-like materials. Am. J. Eng. Appl. Sci., 2010, 3, pp 232–239.CrossRefGoogle Scholar
Mooney, M. A theory of large elastic deformations. J. Appl. Phys., 1940, 11, pp 582–592.CrossRefGoogle Scholar
Rivlin, R.S. Large elastic deformations of isotropic materials: Fundamental concepts. Philos. Trans. R. Soc. A, 1948, 240, pp 459–490.Google Scholar
Hall, W., Mottram, J.T. and Jones, R.P. Finite element simulation of a rolling automotive tyre to understand its transient macroscopic behavior. Proc. Inst. Mech. Eng. D, 2004, 218, pp 1393–1408.CrossRefGoogle Scholar
Naser, B., Kaliske, M. and Andre, M. Durability simulations of elastomeric structures. In Austrell, P.E. and Kari, L. (Eds), Constitutive Models for Rubber IV, AA Balkema Publishers, Rotterdam, Netherlands, 2005, p 45–50.Google Scholar
Shiraishi, M., Iwasaki, N., Saruwatari, T. and Hayashi, K. Developing FE-tyre model library for durability and crash simulations. 7th European LS-DYNA Users’ Conference, Salzburg, May, 2009.Google Scholar
Danielson, K.T., Noor, A.K. and Green, J.S. Computational strategies for tyre modelling and analysis, Comput. Struct., 1996, 61, pp 673–693.CrossRefGoogle Scholar
Wong, J.Y. Theory of Ground Vehicles, 2nd edition, John Wiley & Sons, Inc. New York, 2008.Google Scholar
Clark, S.K. Mechanics of Pneumatic Tires, U.S. Department of Transportation, Washington, DC, 1981.Google Scholar
Federal Aviation Administration, “Aircraft tires”, TSO-C62, Washington, DC, 2006.Google Scholar