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Reduction of circumferential variation in the final stage of IPC
- Authors: Popov G.M.1, Mamedov A.C.1, Smirnova Y.D.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 11, No 3-1 (2012): Special Issue
- Pages: 87-92
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2099
- DOI: https://doi.org/10.18287/2541-7533-2012-0-3-1(34)-87-92
- ID: 2099
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Abstract
Circumferential variation of the flow in final stage rotor wheel, caused by the support racks at the exit of the IPC, is evaluated by means of intermediate pressure of compressor of workflow 3D model. The methods of reducing the circumferential variation of flow by changing final stage’s guide vanes angles.
About the authors
G. M. Popov
Samara State Aerospace University
Author for correspondence.
Email: grishatty@mail.ru
Engineer of the Engine Theory Department
Russian FederationA. C. Mamedov
Samara State Aerospace University
Email: grishatty@mail.ru
Student
Russian FederationY. D. Smirnova
Samara State Aerospace University
Email: pirajock@ya.ru
Student
Russian FederationReferences
- Кулагин, В.В. Теория, расчёт и проектирование авиационных двигателей и энергетических установок [Текст]: учебное пособие / В.В. Кулагин. - М.: Машиностроение, 2002. - 616 с.
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