Large-eddy simulation of compressible turbulent flow in convergent-divergent nozzles with isothermal wall
Author:
Funder
SERB
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference22 articles.
1. Compressibility effects on the growth and structure of homogeneous turbulent shear flow;Blaisdell;J. Fluid Mech.,1993
2. The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers;Bradshaw;J. Fluid Mech.,1974
3. Similarity analysis for turbulent boundary layer with pressure gradient: outer flow;Castillo;AIAA J.,2001
4. A numerical study of turbulent supersonic isothermal-wall channel flow;Coleman;J. Fluid Mech.,1995
5. Compressibility effects and turbulence scalings in supersonic channel flow;Foysi;J. Fluid Mech.,2004
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1. Large-eddy simulation of shock train in convergent-divergent nozzles with isothermal walls;Journal of Turbulence;2024-08-13
2. Empirical equation of the Mach number as a function of the stagnation pressure ratio for a quasi-one-dimensional compressible flow;FME Transactions;2023
3. DNS of compressible turbulent flow in convergent-divergent nozzles with isothermal wall;International Journal of Heat and Fluid Flow;2022-04
4. Effect of Nozzle Geometry on the Flow Dynamics and Resistance Inside and Outside the Cone-Straight Nozzle;ACS Omega;2022-03-08
5. Throat length effect on the flow patterns in off-design conical nozzles;FME Transactions;2022
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