On rare occasion, aircraft tires have burst in flight after being retracted into the wheel well. The burst rapidly releases a high-pressure plume of gas that may cause damage to systems and structure mounted in the wheel well. Since airplanes must be designed to maintain continued safe flight and landing following a tire burst in the wheel well, it is essential that accurate definitions of the plume pressure loads be provided to the airplane structural and systems designers. Existing plume load definitions have been developed over the years from test data and theoretical calculations, but given the very short duration of the event and the complexity of the dynamics involved, it is desired to validate the existing threat definitions through the use of advanced finite element modeling. This paper describes the use of LS-DYNA to accurately predict the pressure plume created from the controlled release of a pressurized tank. This task is considered part of the validation phase. The next step will include the complexities of the deforming tire to quantify the effect of the rapidly changing hole diameter, and to study how the solution diverges from the classical prediction.
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ASME 2005 Pressure Vessels and Piping Conference
July 17–21, 2005
Denver, Colorado, USA
Conference Sponsors:
- Pressure Vessels and Piping Division
ISBN:
0-7918-4189-8
PROCEEDINGS PAPER
Airplane Tire Burst Plume Analysis
Jon Gabrys
Jon Gabrys
The Boeing Company, Philadelphia, PA
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Ryan Lee
The Boeing Company, Philadelphia, PA
Jon Gabrys
The Boeing Company, Philadelphia, PA
Paper No:
PVP2005-71662, pp. 275-279; 5 pages
Published Online:
July 29, 2008
Citation
Lee, R, & Gabrys, J. "Airplane Tire Burst Plume Analysis." Proceedings of the ASME 2005 Pressure Vessels and Piping Conference. Volume 4: Fluid Structure Interaction. Denver, Colorado, USA. July 17–21, 2005. pp. 275-279. ASME. https://doi.org/10.1115/PVP2005-71662
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