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Empirical Model Development for Predicting Shock Response on Composite Materials Subjected to Pyroshock LoadingThe NASA Engineering and Safety Center (NESC) received a request to develop an analysis model based on both frequency response and wave propagation analyses for predicting shock response spectrum (SRS) on composite materials subjected to pyroshock loading. The model would account for near-field environment (approximately 9 inches from the source) dominated by direct wave propagation, mid-field environment (approximately 2 feet from the source) characterized by wave propagation and structural resonances, and far-field environment dominated by lower frequency bending waves in the structure. This document contains appendices to the Volume I report.
Document ID
20150017051
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Gentz, Steven J.
(NASA Langley Research Center Hampton, VA, United States)
Ordway, David O.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Parsons, David S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Garrison, Craig M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rodgers, C. Steven
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Collins, Brian W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2015
Publication Date
July 1, 2015
Publication Information
Publication: NASA Engineering and Safety Center Technical Assessment Report
Subject Category
Composite Materials
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2015-218781/Vol 2/Pt 1
L-22092
NESC-RP-12-00783
Funding Number(s)
WBS: WBS 869021.05.05.09.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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