Large Eddy Simulation of Highly Compressible Jets with Tripped Boundary Layers
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-030-04915-7_44
Reference11 articles.
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2. Gojon, R., Gutmark, E., Mihaescu, M.: On the response of a rectangular supersonic jet to a near-field located parallel flat plate. AIAA Paper, no. 2017-3018 (2017). https://doi.org/10.2514/6.2017-3018
3. Zaman, K.B.M.Q.: Effect of initial boundary-layer state on subsonic jet noise. AIAA J. 50(8), 1784–1795 (2012). https://doi.org/10.2514/1.J051712
4. Bogey, C., Marsden, O., Bailly, C.: Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of $$10^5$$ . J. Fluid Mech. 701, 352–385 (2012). https://doi.org/10.1017/jfm.2012.162
5. Brés, G.A., Ham, F.E., Nichols, J.W., Lele, S.K.: Nozzle wall modeling in unstructured large eddy simulations for hot supersonic jet predictions, AIAA paper, no. 2013-2142 (2013). https://doi.org/10.2514/6.2013-2142
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