Development of a finite element model for comparing metal and composite fuselage section drop testing-Reference-Cited by-同舟云学术

Development of a finite element model for comparing metal and composite fuselage section drop testing

Published:2017-01-06 Issue:4 Volume:22 Page:401-414
ISSN:1358-8265
Container-title:International Journal of Crashworthiness
language:en
Short-container-title:International Journal of Crashworthiness

Author:

Gransden Derek I.¹^ORCID,Alderliesten René¹^ORCID

Affiliation:

1. Aerospace Engineering Department, Structural Integrity and Composites Group, Technical University of Delft, Kluyverweg, LW Delft, The Netherlands

Funder

European Commission

Publisher

Informa UK Limited

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Transportation

Link

https://www.tandfonline.com/doi/pdf/10.1080/13588265.2016.1273987

Reference16 articles.

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3. M. Eiband,Human tolerance to rapidly applied accelerations: A summary of the literature, Tech. Rep. Memeo 5-19-59E, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH, 1959.

4. E. Fasanella and K. Jackson,Best practices for crash modeling and simulation, Tech. Rep. NASA/TM-2002-211944, National Aeronautics and Space Administration, Army Research Lab, Vehicle Technology Directorate, Hampton, VA, 2002.

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