Model operation of thermo elastic deformation at the electrochemical working compressor blades with using method of final elements in the software environment “ANSYS”
- Authors: 1 11, 1 11, 1 11, 1 11
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 5, No 2-1 (2006): Special Issue
- Pages: 104-108
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/308
- DOI: https://doi.org/10.18287/2541-7533-2006-0-2-1(10)-104-108
- ID: 308
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Abstract
The article is devoted to the actual problem of the up-to-date aviation propulsion engineering – the model operation of thermo elastic deformation at the electrochemical working compressor blades. In the article the results of the development work of creation methodology of model operation of thermal load and value calculation of blade deformation by method of final elements in the software environment “Ansys” are presented. Areas of using this method are discussed.
About the authors
1 1
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
References
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