2007-large-eddy-simulation.pdf (4.39 MB)

Large-eddy simulation of twin impinging jets in cross-flow

Download (4.39 MB)
journal contribution
posted on 21.03.2012, 10:14 by Q Li, Gary Page, Jim McGuirk
The flow-field beneath a jet-borne vertical landing aircraft is highly complex and unsteady. large-eddy simulation is a suitable tool to predict both the mean flow and unsteady fluctuations. This work aims to evaluate the suitability of LES by applying it to two multiple jet impingement problems: the first is a simple twin impinging jet in cross-flow, while the second includes a circular intake. The numerical method uses a compressible solver on a mixed element unstructured mesh. The smoothing terms in the spatial flux are kept small by the use of a monitor function sensitive to vorticity and divergence. The WALE subgrid scale model is utilised. The simpler jet impingement case shows good agreement with experiment for mean velocity and normal stresses. Analysis of time histories in the jet shear layer and near impingement gives a dominant frequency at a Strouhal number of 0.1, somewhat lower than normally observed in free jets. The jet impingement case with an intake also gives good agreement with experimental velocity measurements, although the expansion of the grid ahead of the jets does reduce the accuracy in this region. Turbulent eddies are observed entering the intake with significant swirl. This is in qualitative agreement with experimental visualisation. The results show that LES could be a suitable tool when applied to multiple jet impingement with realistic aircraft geometry.

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Citation

LI, Q., PAGE, G.J. and MCGUIRK, J.J., 2007. Large-eddy simulation of twin impinging jets in cross-flow. The Aeronautical Journal, 111 (1117), pp. 195 - 206.

Publisher

© Royal Aeronautical Society

Version

VoR (Version of Record)

Publication date

2007

Notes

This article was published in The Aeronautical Journal [© Royal Aeronautical Society].

ISSN

0001-9240

Language

en

Exports

Logo branding

Exports