Optimization of an Oleo-Pneumatic Shock Absorber for Main Landing Gear of a Commercial Aircraft-Reference-Cited by-同舟云学术

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Optimization of an Oleo-Pneumatic Shock Absorber for Main Landing Gear of a Commercial Aircraft

Published:2017 Issue: Volume: Page:
ISSN:1556-5068
Container-title:SSRN Electronic Journal
language:en
Short-container-title:SSRN Journal

Author:

Patel Jay,Shetty Drithi,Menghani Ritika,Barve Sachin

Publisher

Elsevier BV

Reference12 articles.

1. ?Evaluation of Roughness' in ?Runway Roughness Measurement, Quantification and Application: The BOEING Method;Boeing Commercial Airplane Group

2. Landing Gear Layout Design for Unmanned Aerial Vehicle;Akhilesh Jha;Presented at 14th National Conference on Machines and Mechanisms (NaCoMM09),2009

3. Shock Absorber Design

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. Design, structure analysis and shock control of aircraft landing gear system with MR damper;Smart Materials and Structures;2024-04-25

2. Landing efficiency control of a six degrees of freedom aircraft model with magneto-rheological dampers: Part 2—control simulation;Journal of Intelligent Material Systems and Structures;2020-07-23

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