Turbulence and Aeroacoustics in High-Speed Jets
Speaker: Sanjiva K. Lele, Stanford University
Presentation
Abstract
Engineering applications such as high-speed propulsion or supersonic/hypersonic aerodynamics require accurate predictions of compressible turbulent flows. To improve engineering models for these applications it is helpful to separate variable-density or variable fluid property effects, which dominate the turbulence behavior in supersonic and hypersonic turbulent boundary layers from intrinsic compressibility effects associated with pressure-induced volume change. Highlights from a recent study of compressible shear layers1 are used to stress the close coupling between turbulence and acoustics in such flows, including in high-speed jets. The discussion is then expanded to the problem of predicting the noise radiated by high-speed turbulent jets at pressure-matched and mismatched conditions. Results from recent work using large eddy simulations2,3 are analyzed to characterize the modeling issues faced in predicting turbulent mixing noise, broadband shock-associated noise and jet screech.
[1] Matsuno, K. and Lele, S. K. (2021) J. Fluid Mech. Vol. 907 [2] Bres, G. A. and Lele, S. K. (2019) Phil. Trans. Roy. Soc. A 377:20190081 [3] Wu, G. J., Lele, S. K. and Jeun, J. (2020) CTR Annual Briefs
Biography