Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes

Abstract


The calculation research of the working process of multistage axial turbine in two different software systems was performed. The calculations were performed using an identical geometry, boundary conditions and under the same engine operation conditions. Detailed information about the parameters and structure of the flow in the turbine.


About the authors

O. V. Baturin

Samara State Aerospace University

Author for correspondence.
Email: oleg.v.baturin@gmail.com

Russian Federation

Candidate of Science {Engineering}

Assistant Professor of the Chair of Theory of Engine for Flying Vehicle

M. N. Senchev

Samara State Aerospace University

Email: rider_max@mail.ru

Russian Federation

Magistrand

P. T. Dzhibilov

Samara State Aerospace University

Email: grishatty@mail.ru

Russian Federation

Magistrand

References

  1. Попов, Г.М. Расчётное изучение структуры потока вблизи втулочного сечения в лопаточном венце осевой турбины [Текст] / Г.М. Попов, О.В. Батурин // Вестн. СГАУ. – Самара, 2009. – Вып. 3 (19). – Ч.2. - C. 365-368.
  2. Дмитриева, И.Б. Автоматизация создания объёмной модели пера лопатки в ANSYS Tur-boGrid на базе традиционного представления его геометрии [Текст] / И.Б. Дмитриева, Л.С. Шаблий // Вестн. СГАУ. – Самара, 2011. – Вып. 3 (27). Ч. 3. – С. 106-111.

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