Aircraft Tire Spin-Up Wear Analysis through Experimental Testing and Computational Modeling-Reference-Cited by-同舟云学术

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Aircraft Tire Spin-Up Wear Analysis through Experimental Testing and Computational Modeling

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Zakrajsek Andrew J.¹,Childress Jonathan¹,Bohun Michael H.¹,Naboulsi Sam²,Vogel Ryan N.¹,Lindsey Ned J.²,Mall Shankar³

Affiliation:

1. U.S. Air Force

2. Air Force Research Laboratory

3. Air Force Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0413

Reference26 articles.

1. Initial Identification of Aircraft Tire Wear

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Tyre heat of multi-wheel bogie undercarriage at touchdown;CEAS Aeronautical Journal;2024-03-30

2. Thermal Penetration of Aircraft Tyre Tread at Touchdown;International Journal of Aeronautical and Space Sciences;2024-03-29

3. Temperature elevation of aircraft tyre surface at touchdown with pre-rotations;CEAS Aeronautical Journal;2023-03

4. Iterative Prototyping of Aircraft Tire Wear Measurement Using Laser Profilometer;AIAA Aviation 2019 Forum;2019-06-15

5. The Development and use of a Digital Twin Model for Tire Touchdown Health Monitoring;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

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