E3S Web Conf.
Volume 128, 2019XII International Conference on Computational Heat, Mass and Momentum Transfer (ICCHMT 2019)
|Number of page(s)||3|
|Section||Computational Thermal Fluid Dynamics|
|Published online||08 November 2019|
The numerical simulation of compressible jet at low Reynolds number using OpenFOAM
Ivannikov Institute for System Programming of the RAS,
Solzhenitsyna str., 25,
2 Keldysh Institute of Applied Mathematics of the RAS, 125047, Miusskaya pl., 4, Moscow, Russia
3 Bauman Moscow State Technical University, 105005, 2-aya Baumanskaya str., 5, Moscow, Russia
4 Department of Aeromechanics and Flight Engineering of MIPT, 140180, Gagarina str., 16, Zhukovsky, Russia
* Corresponding author: firstname.lastname@example.org
The paper presents an analysis of various approaches for calculation gas-dynamic parameters and acoustic perturbations generated by a compressible jet at low Reynolds number (M = 0.9, Re = 3600). The jet flow parameters at selected conditions are well studied and can be used for validation of the numerical methods and schemes. The OpenFOAM software package with various approaches (solvers) such as pimpleCentralFoam, dbnsTurbFoam and new QGDFoam solver based on QGD-algorithms are considered. The results of time-averaged flow parameters and acoustic properties are compared with the experimental data. To determine the acoustic perturbation the Ffowcs Williams and Hawkings analogy implemented in our OpenFOAM library (libAcoustic) has been used.
© The Authors, published by EDP Sciences, 2019
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