Design optimisation and experimental verification of a UAV’s landing gear buffer-Reference-Cited by-同舟云学术

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Design optimisation and experimental verification of a UAV’s landing gear buffer

Published:2023-08-01 Issue: Volume: Page:1-10
ISSN:1358-8265
Container-title:International Journal of Crashworthiness
language:en
Short-container-title:International Journal of Crashworthiness

Author:

Chen Jinjin¹,Xue Caijun¹

Affiliation:

1. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Publisher

Informa UK Limited

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Transportation

Link

https://www.tandfonline.com/doi/pdf/10.1080/13588265.2023.2242102

Reference22 articles.

1. Towards the Unmanned Aerial Vehicles (UAVs): A Comprehensive Review

2. Shock and harmonic response analysis of UAV nose landing gear system with air damper

3. Crashworthiness study of UCAV’s main landing gear using explicit dynamics

Cited by 2 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. The Effect of Landing Gear Dimension Variation on the Static Strength and Dynamic Response of Unmanned Aerial Vehicle (UAV);International Journal of Automotive and Mechanical Engineering;2023-10-18

2. Effect of Metallic Coatings on the Wear Performance and Mechanism of 30CrMnSiNi2A Steel;Materials;2023-09-13

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