2018
DOI: 10.3390/app8040593
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Finite Element Modeling of an Aircraft Tire Rolling on a Steel Drum: Experimental Investigations and Numerical Simulations

Abstract: The aim of this study is to investigate the thermal evolution of an aircraft tire rolling at high velocities up to take off values. As this kind of experiment is difficult to realize on a real runway, experimental tests were realized on aircraft tires rolling on a steel drum. The rotating drum facility allows to apply variable velocities beyond the take off limits, at fixed skidding angles and loadings. The rolling conditions, vertical loading, velocity and cornering conditions were adopted to correspond to th… Show more

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Cited by 12 publications
(6 citation statements)
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“…This is particularly true when prototyping or testing is not easy to perform due to the difficulty of measuring or performance limits of the equipment. Rosu et al used the finite element tire model to predict the temperature change inside the tire until the time of takeoff of the airplane tire [ 11 ]. Behroozinia et al proposed the possibility of detecting cracks inside the tire through analysis of the acceleration signal measured inside the tire using rolling simulations of the finite element tire model [ 12 ].…”
Section: Related Materialsmentioning
confidence: 99%
“…This is particularly true when prototyping or testing is not easy to perform due to the difficulty of measuring or performance limits of the equipment. Rosu et al used the finite element tire model to predict the temperature change inside the tire until the time of takeoff of the airplane tire [ 11 ]. Behroozinia et al proposed the possibility of detecting cracks inside the tire through analysis of the acceleration signal measured inside the tire using rolling simulations of the finite element tire model [ 12 ].…”
Section: Related Materialsmentioning
confidence: 99%
“…During the spin-up phase, the skidding of the tyres generates enough heat to burn the tyres and may cause the contact patch of the tyre to revert to its uncured state (Wu et al , 2019). This reverted rubber cannot be cooled in the short spin-up time (Linke et al , 2014), hence the directional control of the aircraft or its braking performance during the second phase can be affected by the temperature of the tyres (Rosu et al , 2016; Rosu et al , 2018). Therefore, we conclude that, during the spin-up period, preventing the increase of tyre temperature is more important than reducing their wear.…”
Section: Review Of the Tyre Wear Characteristics During Aircraft Landingmentioning
confidence: 99%
“…Because of the complicated nature, it is difficult to establish a function to describe the relationship between sensor output and sensor parameters. Thus, finite element analysis [21][22][23] was used to calculate the sensor responses.…”
Section: Simulation and Analysismentioning
confidence: 99%