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Development of numerical models of working process in fuel auger-centrifugal pump
- Authors: Gafurov S.A.1, Miheev M.G.2, Rodionov L.V.1, Kruchkov A.N.1, Shahmatov E.V.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolev (National Research University)
- JSC «KUZNETSOV»
- Issue: Vol 10, No 3-4 (2011): Special Issue
- Pages: 254-263
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/7001
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-4(27)-254-263
- ID: 7001
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Abstract
The issues compiling numerical computational model based on the method of finite volumes are discussed in this paper. This model is used to measure axial force acting on the rotor of auger-centrifugal stage of combined fuel pump. Model verified by comparing the calculated and experimental characteristics of the discharge. The paper discusses the impact of some design parameters auger-centrifugal stage on the value of the axial force.
About the authors
S. A. Gafurov
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Author for correspondence.
Email: sa.gafurov@gmail.com
graduated student
Russian FederationM. G. Miheev
JSC «KUZNETSOV»
Email: mecmod@mail.ru
design engineer
Russian FederationL. V. Rodionov
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Email: rl63@bk.ru
Candidate of Technical Sciences
assistant
A. N. Kruchkov
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Email: kan@ssau.ru
Doctor of Engineering, associated professor
Russian FederationE. V. Shahmatov
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Email: shakhm@ssau.ru
Doctor of Engineering, professor
Russian FederationReferences
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