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DETERMINING GEOMETRICAL PARAMETERS OF CENTRIPETAL MICROTURBINE NOZZLE CONSISTING OF RECTILINEAR BLADES
- Authors: Mussatkin N.F.1, Radko V.M.1, Balakhonov A.D.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 2, No 1 (2003)
- Pages: 106-110
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/6982
- DOI: https://doi.org/10.18287/2541-7533-2003-0-1%20(3)-106-110
- ID: 6982
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Abstract
A procedure for determining structural geometrical parameters of nozzle blade profiles on the basis of the results of gas-dynamic calculation of a stage of a radial centripetal microturbine is presented.
About the authors
N. F. Mussatkin
Samara State Aerospace University
Author for correspondence.
Email: vest@ssau.ru
Russian Federation
V. M. Radko
Samara State Aerospace University
Email: vest@ssau.ru
Russian Federation
A. D. Balakhonov
Samara State Aerospace University
Email: vest@ssau.ru
Russian Federation
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