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Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT
- Authors: Baturin N.V.1, Baturin O.V.1, Matveev V.N.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 8, No 3-1 (2009): Special Issue
- Pages: 298-304
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/712
- DOI: https://doi.org/10.18287/2541-7533-2009-0-3-1(19)-298-304
- ID: 712
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Abstract
Article is devoted to a formation of a structural calculated finite element mesh of the passage blade of the axial turbine in program Gambit. Possible ways of construction of calculated model in the program are considered, the analysis on basis of what the new way allowing to create a better structural mesh has been offered, thereby to raise accuracy of calculation.
About the authors
N. V. Baturin
Samara State Aerospace University
Author for correspondence.
Email: oleg.v.baturin@gmail.com
Russian Federation
O. V. Baturin
Samara State Aerospace University
Email: oleg.v.baturin@gmail.com
Russian Federation
V. N. Matveev
Samara State Aerospace University
Email: matveev.vn@ssau.ru
Russian Federation
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