Effect of preloaded state slat structure on the stress–strain state of simulation bird strike-Reference-Cited by-同舟云学术

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Effect of preloaded state slat structure on the stress–strain state of simulation bird strike

Published:2023-06-30 Issue: Volume: Page:
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Olga Rod,Oleg Molkov,Nikita Lutsenko,Aleksandr Bolshikh,Anna Storchak

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-023-00236-3.pdf

Reference21 articles.

1. EASA (2007) Certification specification for large aeroplanes CS-25. EASA, Brussels

2. FAA (2010) Electronic code of federal regulations: FAR-25. FAA, Washington, D.C.

3. Zhang J, Ning HS, Liu J et al (2008) Bird situations and bird strike risks in Chinese civil airports. Aviation 86(2):73–76

4. Mao RH, Meguid SA, Ng TY (2006) Finite element modeling of a bird striking an engine fan blade. AIAA 44:583–596

5. ABAQUS (2008) Analysis User Manual, Version 6.8. Dassault Systémes

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. Development and Validation of a Finite Element Model for Bird Strike Test;ANNUAL JOURNAL OF TECHNICAL UNIVERSITY OF VARNA, BULGARIA;2024-06-28

2. Theoretical Model of the Methodology of Landing Gear Bracket Design Taking into Account the Adjusted Calculation for Shear Bolt Design;E3S Web of Conferences;2023

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