Reliability Analysis of Landing Gear Retraction System Influenced by Multifactors-Reference-Cited by-同舟云学术

Reliability Analysis of Landing Gear Retraction System Influenced by Multifactors

Published:2016-05 Issue:3 Volume:53 Page:713-724
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Yin Yin¹,Hong Nie¹,Huajin Ni¹,Ming Zhang¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033333

Reference26 articles.

1. Aircraft Landing Gear Design: Principles and Practices

2. Aircraft Design Manual Book 14: Taking-Off and Landing Devices Design, Committee of Aircraft Design Manual, Aviation Industry Press, Beijing, 2002, pp. 442–465 (in Chinese).

3. CAD embedded CAE tools for aircraft designers as applied to landing gear

4. New design procedures applied to landing gear development

5. ReveleyM. S.BriggsJ. L.EvansJ. K.JonesS. M.KurtogluT.LeoneK. M.SandiferC. E. “Causal Factors and Adverse Events of Aviation Accidents and Incidents Related to Integrated Vehicle Health Management,” Aviation Safety Reporting System, 2011.

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