Evaluation of fatigue damage accumulation functions for delamination initiation and propagation /

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Bibliographic Details
Author / Creator:Davila, Carlos G., author.
Imprint:Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2020.
Description:1 online resource (ii, 32 pages, 1 unnumbered page) : color illustrations.
Language:English
Series:NASA/TP ; 2020-220584
NASA technical publication ; 2020-220584.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12696007
Hidden Bibliographic Details
Other authors / contributors:Langley Research Center, issuing body.
Notes:"April 2020."
Includes bibliographical references (pages 31-32).
Technical publication.
NASA Langley Research Center 081876.02.07.18.01.03.02
Description based on online resource, PDF version; title from title page (NASA, viewed on Jan. 28, 2021).
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:2020-220584

MARC

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588 |a Description based on online resource, PDF version; title from title page (NASA, viewed on Jan. 28, 2021). 
650 0 |a Composite materials  |x Delamination.  |0 http://id.loc.gov/authorities/subjects/sh89000016 
650 7 |a Crack propagation.  |2 nasat 
650 7 |a Fatigue life.  |2 nasat 
650 7 |a Cyclic loads.  |2 nasat 
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