Hydrodynamic ram analysis of aircraft fuel tanks with different composite T-joint designs
Author:
Affiliation:
1. Airbus Group Innovations (formerly EADS Innovation Works), Munich, Germany
2. WIWeB, Bundeswehr Research Institute for Materials, Fuels and Lubricants, Germany
Publisher
WIT Press
Link
http://www.witpress.com/Secure/elibrary/papers/SUSI14/SUSI14024FU1.pdf
Cited by 7 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. Predicting Hydrodynamic RAM Damage in Bonded Composite Tanks Using Progressive Damage Failure Analysis;AIAA Scitech 2020 Forum;2020-01-05
2. Numerical study on the impact response of aircraft fuselage structures subjected to large-size tire fragment;Science Progress;2019-09-27
3. Numerical Analysis of a Bonded Composite T Joint Subjected to Hydrodynamic Ram Pressures in a Ramgun;AIAA Scitech 2019 Forum;2019-01-06
4. Investigation of Hydrodynamic Ram Behavior Using Newly Established HRam Gun System;International Journal of Aeronautical and Space Sciences;2018-10-17
5. Analysis of the mechanical behavior of composite T-joints reinforced by one side stitching;Composite Structures;2018-01
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