Effect of the Mechanical and Thermal Stresses of Rotating Blades
Rotating blades are the important parts in gas turbines. Hence, an accurate mathematical estimation (F.E.M) of the stresses and deformations characteristics was required in the design applications to avoid failure. In recent years there are researchers interest in the effect of temperature on solid...
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Al-Khwarizmi College of Engineering – University of Baghdad
2007
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oai:doaj.org-article:4b22d69df1c94ea9a7d73be5c745b91e2021-12-02T01:53:29ZEffect of the Mechanical and Thermal Stresses of Rotating Blades1818-1171https://doaj.org/article/4b22d69df1c94ea9a7d73be5c745b91e2007-01-01T00:00:00Zhttp://www.iasj.net/iasj?func=fulltext&aId=2342https://doaj.org/toc/1818-1171Rotating blades are the important parts in gas turbines. Hence, an accurate mathematical estimation (F.E.M) of the stresses and deformations characteristics was required in the design applications to avoid failure. In recent years there are researchers interest in the effect of temperature on solid bodies has greatly increased, The main of this study investigated the thermal and rotational effects. So, the thermal stresses due to high pressure and temperature are studies, also determine the steady state stresses and deformations of rotating blades due to mechanical effect. Many parameters such as thickness and centre of rotating are investigated in this paper. The study results can ensure good recommendation for the effect of the mechanical and thermal stresses of rotary blades. Malik M. Ali. Nabeel K. AL-sahibAl-Khwarizmi College of Engineering – University of BaghdadarticleThermal StressesFinite Element MethodMechanical StressesBlade MaterialDesign .Chemical engineeringTP155-156Engineering (General). Civil engineering (General)TA1-2040ENAl-Khawarizmi Engineering Journal, Vol 3, Iss 2, Pp 32-48 (2007) |
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topic |
Thermal Stresses Finite Element Method Mechanical Stresses Blade Material Design . Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 |
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Thermal Stresses Finite Element Method Mechanical Stresses Blade Material Design . Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 Malik M. Ali . Nabeel K. AL-sahib Effect of the Mechanical and Thermal Stresses of Rotating Blades |
description |
Rotating blades are the important parts in gas turbines. Hence, an accurate mathematical estimation (F.E.M) of the stresses and deformations characteristics was required in the design applications to avoid failure. In recent years there are researchers interest in the effect of temperature on solid bodies has greatly increased, The main of this study investigated the thermal and rotational effects. So, the thermal stresses due to high pressure and temperature are studies, also determine the steady state stresses and deformations of rotating blades due to mechanical effect. Many parameters such as thickness and centre of rotating are investigated in this paper. The study results can ensure good recommendation for the effect of the mechanical and thermal stresses of rotary blades. |
format |
article |
author |
Malik M. Ali . Nabeel K. AL-sahib |
author_facet |
Malik M. Ali . Nabeel K. AL-sahib |
author_sort |
Malik M. Ali |
title |
Effect of the Mechanical and Thermal Stresses of Rotating Blades |
title_short |
Effect of the Mechanical and Thermal Stresses of Rotating Blades |
title_full |
Effect of the Mechanical and Thermal Stresses of Rotating Blades |
title_fullStr |
Effect of the Mechanical and Thermal Stresses of Rotating Blades |
title_full_unstemmed |
Effect of the Mechanical and Thermal Stresses of Rotating Blades |
title_sort |
effect of the mechanical and thermal stresses of rotating blades |
publisher |
Al-Khwarizmi College of Engineering – University of Baghdad |
publishDate |
2007 |
url |
https://doaj.org/article/4b22d69df1c94ea9a7d73be5c745b91e |
work_keys_str_mv |
AT malikmali effectofthemechanicalandthermalstressesofrotatingblades AT nabeelkalsahib effectofthemechanicalandthermalstressesofrotatingblades |
_version_ |
1718402833455251456 |