Application of Progressive Damage Failure Analysis to Large Aircraft Composite Structures-Reference-Cited by-同舟云学术

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Application of Progressive Damage Failure Analysis to Large Aircraft Composite Structures

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Selvarathinam Alex S.¹,Stewart Mark W.¹,Engelstad Stephen P.¹,Eby Brandon¹

Affiliation:

1. Lockheed Martin Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2235

Reference4 articles.

1. Virtual testing of realistic aerospace composite structures

2. 4Norwood, D.S., Gail, L.H., Joyce, P.F., Wippich-Dienhart, R.J. "Historical Assessment of Building Block Development Test Programs for Modern Military Aircraft (AIAA 2016-0231).

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1. Test Methodology Establishment of Hydrodynamic Ram Effect on Aircraft Wing Fuel Tank;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18

2. Revisiting Building Block Approaches for Structures;AIAA SCITECH 2022 Forum;2022-01-03

3. Predicting Hydrodynamic RAM Damage in Bonded Composite Tanks Using Progressive Damage Failure Analysis;AIAA Scitech 2020 Forum;2020-01-05

4. Investigation of Hydrodynamic Ram Behavior Using Newly Established HRam Gun System;International Journal of Aeronautical and Space Sciences;2018-10-17

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