Научная визуализация

Scientific Visualization

Электронный журнал открытого доступа

Национальный Исследовательский Ядерный Университет "МИФИ"

      ISSN 2079-3537      

 
 
 
                                                                                                                                                                                                                                                                                                                                                                                                                                                                             





Научная визуализация, 2020, том 12, номер 4, страницы 46 - 55, DOI: 10.26583/sv.12.4.05

Аpplication of scientific visualization tools in the study of supersonic vortex pair

Авторы: V.E. Borisov1, A.A. Davydov2, T.V. Konstantinovskaya3, A.E.  Lutsky4

Keldysh Institute of Applied Mathematics RAS

1 ORCID: 0000-0003-4448-7474, narelen@gmail.com

2 ORCID: 0000-0001-5662-817X, ryzhiy@list.ru

3 ORCID: 0000-0002-1127-503X, konstantinovskaya.t.v@gmail.com

4 ORCID: 0000-0002-4442-0571, allutsky@yandex.ru

 

Аннотация

Scientific visualization is an important stage of research. It is intended to provide post-processing analysis tools for presenting the results obtained numerically and/or experimentally. This is especially topical with regard to the increasing volume of processed data associated with the productive capacity growth of computing systems.

In this work two scientific visualization methods were applied to recognize flow parameters obtained by numerical simulation of counter-rotating supersonic vortex pair interaction: the λ2-method and maximum vorticity method.

The results of their application are compared. The numerical data was obtained by a computational model based on the URANS equations with SA turbulence model. Numerical simulations were performed on the hybrid supercomputing system K-60 at the Keldysh Institute of Applied Mathematics RAS. The main simulation results are presented and analyzed.

 

Ключевые слова: supersonic flow, vortex flow, counter-rotating pair, scientific visualization.