Eintrag weiter verarbeiten

Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy

Gespeichert in:

Bibliographische Detailangaben
Zeitschriftentitel: AIAA Journal
Personen und Körperschaften: Manjunatha, C. M., Parida, B. K.
In: AIAA Journal, 42, 2004, 8, S. 1536-1542
Format: E-Article
Sprache: Englisch
veröffentlicht:
American Institute of Aeronautics and Astronautics (AIAA)
Schlagwörter:
author_facet Manjunatha, C. M.
Parida, B. K.
Manjunatha, C. M.
Parida, B. K.
author Manjunatha, C. M.
Parida, B. K.
spellingShingle Manjunatha, C. M.
Parida, B. K.
AIAA Journal
Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
Aerospace Engineering
author_sort manjunatha, c. m.
spelling Manjunatha, C. M. Parida, B. K. 0001-1452 1533-385X American Institute of Aeronautics and Astronautics (AIAA) Aerospace Engineering http://dx.doi.org/10.2514/1.880 Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy AIAA Journal
doi_str_mv 10.2514/1.880
facet_avail Online
finc_class_facet Technik
format ElectronicArticle
fullrecord blob:ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMjUxNC8xLjg4MA
id ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMjUxNC8xLjg4MA
institution DE-Gla1
DE-Zi4
DE-15
DE-Pl11
DE-Rs1
DE-105
DE-14
DE-Ch1
DE-L229
DE-D275
DE-Bn3
DE-Brt1
DE-D161
imprint American Institute of Aeronautics and Astronautics (AIAA), 2004
imprint_str_mv American Institute of Aeronautics and Astronautics (AIAA), 2004
issn 0001-1452
1533-385X
issn_str_mv 0001-1452
1533-385X
language English
mega_collection American Institute of Aeronautics and Astronautics (AIAA) (CrossRef)
match_str manjunatha2004predictionoffatiguecrackgrowthaftersingleoverloadinanaluminumalloy
publishDateSort 2004
publisher American Institute of Aeronautics and Astronautics (AIAA)
recordtype ai
record_format ai
series AIAA Journal
source_id 49
title Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_unstemmed Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_full Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_fullStr Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_full_unstemmed Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_short Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_sort prediction of fatigue crack growth after single overload in an aluminum alloy
topic Aerospace Engineering
url http://dx.doi.org/10.2514/1.880
publishDate 2004
physical 1536-1542
description
container_issue 8
container_start_page 1536
container_title AIAA Journal
container_volume 42
format_de105 Article, E-Article
format_de14 Article, E-Article
format_de15 Article, E-Article
format_de520 Article, E-Article
format_de540 Article, E-Article
format_dech1 Article, E-Article
format_ded117 Article, E-Article
format_degla1 E-Article
format_del152 Buch
format_del189 Article, E-Article
format_dezi4 Article
format_dezwi2 Article, E-Article
format_finc Article, E-Article
format_nrw Article, E-Article
_version_ 1792344434694684673
geogr_code not assigned
last_indexed 2024-03-01T17:07:31.598Z
geogr_code_person not assigned
openURL url_ver=Z39.88-2004&ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fvufind.svn.sourceforge.net%3Agenerator&rft.title=Prediction+of+Fatigue+Crack+Growth+After+Single+Overload+in+an+Aluminum+Alloy&rft.date=2004-08-01&genre=article&issn=1533-385X&volume=42&issue=8&spage=1536&epage=1542&pages=1536-1542&jtitle=AIAA+Journal&atitle=Prediction+of+Fatigue+Crack+Growth+After+Single+Overload+in+an+Aluminum+Alloy&aulast=Parida&aufirst=B.+K.&rft_id=info%3Adoi%2F10.2514%2F1.880&rft.language%5B0%5D=eng
SOLR
_version_ 1792344434694684673
author Manjunatha, C. M., Parida, B. K.
author_facet Manjunatha, C. M., Parida, B. K., Manjunatha, C. M., Parida, B. K.
author_sort manjunatha, c. m.
container_issue 8
container_start_page 1536
container_title AIAA Journal
container_volume 42
description
doi_str_mv 10.2514/1.880
facet_avail Online
finc_class_facet Technik
format ElectronicArticle
format_de105 Article, E-Article
format_de14 Article, E-Article
format_de15 Article, E-Article
format_de520 Article, E-Article
format_de540 Article, E-Article
format_dech1 Article, E-Article
format_ded117 Article, E-Article
format_degla1 E-Article
format_del152 Buch
format_del189 Article, E-Article
format_dezi4 Article
format_dezwi2 Article, E-Article
format_finc Article, E-Article
format_nrw Article, E-Article
geogr_code not assigned
geogr_code_person not assigned
id ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMjUxNC8xLjg4MA
imprint American Institute of Aeronautics and Astronautics (AIAA), 2004
imprint_str_mv American Institute of Aeronautics and Astronautics (AIAA), 2004
institution DE-Gla1, DE-Zi4, DE-15, DE-Pl11, DE-Rs1, DE-105, DE-14, DE-Ch1, DE-L229, DE-D275, DE-Bn3, DE-Brt1, DE-D161
issn 0001-1452, 1533-385X
issn_str_mv 0001-1452, 1533-385X
language English
last_indexed 2024-03-01T17:07:31.598Z
match_str manjunatha2004predictionoffatiguecrackgrowthaftersingleoverloadinanaluminumalloy
mega_collection American Institute of Aeronautics and Astronautics (AIAA) (CrossRef)
physical 1536-1542
publishDate 2004
publishDateSort 2004
publisher American Institute of Aeronautics and Astronautics (AIAA)
record_format ai
recordtype ai
series AIAA Journal
source_id 49
spelling Manjunatha, C. M. Parida, B. K. 0001-1452 1533-385X American Institute of Aeronautics and Astronautics (AIAA) Aerospace Engineering http://dx.doi.org/10.2514/1.880 Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy AIAA Journal
spellingShingle Manjunatha, C. M., Parida, B. K., AIAA Journal, Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy, Aerospace Engineering
title Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_full Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_fullStr Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_full_unstemmed Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_short Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
title_sort prediction of fatigue crack growth after single overload in an aluminum alloy
title_unstemmed Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
topic Aerospace Engineering
url http://dx.doi.org/10.2514/1.880