The Inductive Method of Landing Shock Data of Aero-engine and Shock Characteristics Analysis-Reference-Cited by-同舟云学术

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The Inductive Method of Landing Shock Data of Aero-engine and Shock Characteristics Analysis

Published:2020-10-14 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of the 2020 International Conference on Aviation Safety and Information Technology
language:
Short-container-title:

Author:

Wang Qian¹,Lei Xiaobo²

Affiliation:

1. Chinese Flight Test Establishment, Xi'an, China

2. Xi'an Aeronautical University Xi'an, China

Publisher

ACM

Link

https://dl.acm.org/doi/pdf/10.1145/3434581.3434622

Reference18 articles.

1. Research on the impact response spectrum of fixed-wing aircraft external objects landing[J];Xiaobo Lei;Flight Mechanics,2015

2. Analysis of landing gear landing dynamics based on the concept of landing zone[J];Xiaohui Wei;Acta Aeronautica Sinica,2005

3. The response of materials and structures under impact load[J];Tongxi Yu;Advances in Mechanics,1997

4. The response of materials and structures under impact load[J];Tongxi Yu;Advances in Mechanics,1997

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