“…[39,40] The procedure employed for parallelization has been demonstrated to be portable, due to the use of the standardized MPI library. FDL3DI has been utilized successfully on a number of different computing platforms, and has maintained a parallel efficiency of 90% for up to 320 processors.…”
Section: Validation Of the Numerical Methodsmentioning
confidence: 99%
“…A summary of these may be found in Ref. [40]. For the simulations presented here, we consider a deep cavity where the length to depth ratio is less than 9.…”
Section: Acoustic Suppression Of Supersonic Cavity Flowmentioning
“…[39,40] The procedure employed for parallelization has been demonstrated to be portable, due to the use of the standardized MPI library. FDL3DI has been utilized successfully on a number of different computing platforms, and has maintained a parallel efficiency of 90% for up to 320 processors.…”
Section: Validation Of the Numerical Methodsmentioning
confidence: 99%
“…A summary of these may be found in Ref. [40]. For the simulations presented here, we consider a deep cavity where the length to depth ratio is less than 9.…”
Section: Acoustic Suppression Of Supersonic Cavity Flowmentioning
“…Y [3] tested the rationality of the application of he KSKL-SAS and the SST-SAS model in the aerodynamic noise. Donald P. Rizzetta [4] performed the supersonic cavity using a high-order large-eddy simulation. Moreover, a active flow control could be applied by pulsed mass injection to suppress noise.…”
“…A similar study was carried out experimentally by Zhuang, et.al [4] and a numerical investigation of approximately similar geometry using LES turbulence model was carried out by Rizzetta, et.al [5].…”
Section: Grid and Solutionsmentioning
confidence: 96%
“…The grid is shown for every other point in Figure 1. The freestream flow conditions are Mach=2.0, P 0 =2.17x10 5 Pa, and T 0 =336 K, Re/cm=2.33x10 5 . The unsteady cavity solutions were obtained with symmetric and full configurations with and without control to investigate the asymmetric effect of the turbulence model.…”
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