Multigrid Algorithm for Computing Hypersonic, Chemically Reacting Flows

2001 ◽  
Vol 38 (6) ◽  
pp. 865-874 ◽  
Author(s):  
Sung-Soo Kim ◽  
Chongam Kim ◽  
Oh-Hyun Rho
Keyword(s):  
Reacting Flows ◽  
Multigrid Algorithm ◽  
Chemically Reacting Flows ◽  
Chemically Reacting

Three-dimensional upwind, parabolized Navier-Stokes code for chemically reacting flows

10.2514/3.261 ◽  
1991 ◽  
Vol 5 (3) ◽  
pp. 274-283 ◽  
Author(s):  
Philip E. Buelow ◽  
John C. Tannehill ◽  
John O. levalts ◽  
Scott L. Lawrence
Keyword(s):  
Three Dimensional ◽  
Reacting Flows ◽  
Navier Stokes ◽  
Chemically Reacting Flows ◽  
Chemically Reacting

Upwind parabolized Navier-Stokes code for chemically reacting flows

10.2514/3.157 ◽  
1990 ◽  
Vol 4 (2) ◽  
pp. 149-156 ◽  
Author(s):  
John C. Tannehill ◽  
John O. Ievalts ◽  
Philip E. Buelow ◽  
Dinesh K. Prabhu ◽  
Scott L. Lawrence
Keyword(s):  
Reacting Flows ◽  
Navier Stokes ◽  
Chemically Reacting Flows ◽  
Chemically Reacting

Numerical Simulation of Heat Transfer and Fluid Dynamics in Supersonic Chemically Reacting Flows

2010 ◽  
Author(s):  
Alexander M. Molchanov ◽  
Anna A. Arsentyeva
Keyword(s):  
Heat Transfer ◽  
Fluid Dynamics ◽  
High Speed ◽  
Stokes Equations ◽  
Order Approximation ◽  
Reacting Flows ◽  
Supersonic Combustion ◽  
Special Method ◽  
Chemically Reacting Flows ◽  
Chemically Reacting

An implicit fully coupled numerical method for modeling of chemically reacting flows is presented. Favre averaged Navier-Stokes equations of multi-component gas mixture with nonequilibrium chemical reactions using Arrhenius chemistry are applied. A special method of splitting convective fluxes is introduced. This method allows for using spatially second-order approximation in the main flow region and of first-order approximation in regions with discontinuities. To consider the effects of high-speed compressibility on turbulence the author suggests a correction for the model, which is linearly dependent on Mach turbulent number. For the validation of the code the described numerical procedures are applied to a series of flow and heat and mass transfer problems. These include supersonic combustion of hydrogen in a vitiated air, chemically reacting flow through fluid rocket nozzle, afterburning of fluid and solid rocket plumes, fluid dynamics and convective heat transfer in convergent-divergent nozzle. Comparison of the simulation with available experimental data showed a good agreement for the above problems.

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