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Prediction of Fatigue Crack Growth After Single Overload in an Aluminum Alloy
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Zeitschriftentitel: | AIAA Journal |
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Personen und Körperschaften: | , |
In: | AIAA Journal, 42, 2004, 8, S. 1536-1542 |
Format: | E-Article |
Sprache: | Englisch |
veröffentlicht: |
American Institute of Aeronautics and Astronautics (AIAA)
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Schlagwörter: |
author_facet |
Manjunatha, C. M. Parida, B. K. Manjunatha, C. M. Parida, B. K. |
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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 |
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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 |
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author | Manjunatha, C. M., Parida, B. K. |
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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 |