Journals / International Journal of Automotive Engineering and Technologies / 2015 / Cilt: 4 - Sayı: 1

Flow features of confined swirling jets

Pages
12–15
Publication Date
2022-10-18
DOI
—
🏛️Bibliographic metadata and full text access for this article are provided via DergiPark.
DergiPark Record ↗
✨

AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

To sum up, LES models provide more information thanconventional RANS models and it is a step forward in any research team to gain an insight ofany transitional or fully turbulent process.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:Assessment of LES models of confined coaxial swirling jets is the aim of this paper.
📊
Key Findings & Data:Kernel cores areidentified based on the lambda2 parameter.
💡
Conclusion & Impact:To sum up, LES models provide more information thanconventional RANS models and it is a step forward in any research team to gain an insight ofany transitional or fully turbulent process.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Domain Parameters

Abstract

Assessment of LES models of confined coaxial swirling jets is the aim of this paper. Despitethe simple geometrical set- up of the benchmark, the flow pattern shows complex aerodynamicbehavior. The case considers two coaxial jets: one axial and another annular swirling jet. Theexpansion when entering the chamber will produce the Outer Recirculation Zone (ORZ). Ifswirl number is large enough, an Inner Recirculation Zone (IRZ) is formed. The regionbetween both recirculation zones with high shear is where mixture occurs. Post - process inspace and frequency domain supplies useful information of this benchmark. Kernel cores areidentified based on the lambda2 parameter. The mesh must be fine enough to capture theinertial regime of the turbulent energy spectrum. Proper Orthogonal Decomposition letidentify main flow structures. To sum up, LES models provide more information thanconventional RANS models and it is a step forward in any research team to gain an insight ofany transitional or fully turbulent process.

🔖

Cite This Article

PARRA, T., PEREZ, R., VUORİNEN, V., RODRİGUEZ, M. -. A., CASTRO, F. (2022). Flow features of confined swirling jets. International Journal of Automotive Engineering and Technologies, Cilt: 4 - Sayı: 1, 12–15. https://ajindex.com/articles/540388

📄 Full Text PDF Viewer

📄

PDF görüntüleyici hazırlanıyor...

References (2)

  1. T. Parra, V. Vuorinen, R. Perez, R. Szasz and F. Castro "Aerodynamic characterization of isothermal swirling flows in combustors". International Journal of Energy and Environmental Engineering 5:85. 2014
  2. Roback R., Johnson B.V. Mass and momentum turbulent transport experiments with confined swirling coaxial jets, NASA CR- 168252, 1983 3. L. Davidson “Hybrid LES - RANS: Inlet Boundary Conditions for F lows Including Recirculation” 5th International Symposium on Turbulence and Shear Flow Phenomena TU Munich, Vol. 2, pp. 689–694, 2007 4. V. Vuorinen, M. Larmi, P. Schlatter, L. Fuchs, and B.J. Boersma “A Low- Dissipative, Scale- Selective Discretization Scheme for the Navier- Stokes Equations" Computers & Fluids. 70 (2012) 195–205 5. V. Vuorinen, J. - P. Keskinen, C. Duwig, O. Kaario, J. Yu, M. Larmi, and B.J. Boersma “Finite Volume Implementation of Navier- Stokes Solvers for a Variety of Flow Conditions in Open Source Environment”. Computers & Fluids. 2012 6. R. E. Bensow and G. Bark “Simulating Cavitating Flows with LES in OpenFoam”. V European Conference on Computational Fluid Dynamics ECCOMAS CFD 2010 7. T. Parra- Santos; R. J Pérez- Domínguez; R, Z Szasz; F. Castro. An is othermal analysis of curved- vane and flat - vane swirlers for burners. Engineering Computations. Manuscript accepted for publication on 14- 07- 2014.