The flow hydrodynamic effects and film cooling effectiveness placing two small coolant ports just upstream the main jet (combined triple jets) were numerically investigated. Cross sections of all jets are rectangular and they are inclined normally into the hot cross-flow. The finite volume method and the SIMPLE algorithm on a multiblock nonuniform staggered grid were applied. The large-eddy simulation approach with three different subgrid scale models was used. The obtained results showed that this flow configuration reduces the mixing between the freestream and the coolant jets and hence provides considerable improvements in film cooling effectiveness (both centerline and spanwise averaged effectiveness). Moreover, the effects of density and velocity differences between the jets and cross-flow and between each of the jets were investigated. The related results showed that any increase in density ratio will increase the penetration of the jet into the cross-flow, but increasing the density ratio also increases the centerline and spanwise average film cooling effectiveness. Increasing the smaller jet velocity ratios, compared with the main jet, significantly improve the cooling effectiveness and uniform coolant distribution over the surface by keeping the main jet coolant fluid very close to the wall.
Skip Nav Destination
e-mail: ramezanizadeh@mech.sharif.ir
Article navigation
March 2011
Research Papers
Compound Triple Jets Film Cooling Improvements via Velocity and Density Ratios: Large Eddy Simulation
R. Farhadi-Azar,
R. Farhadi-Azar
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334
Search for other works by this author on:
M. Ramezanizadeh,
M. Ramezanizadeh
Department of Aerospace Engineering,
e-mail: ramezanizadeh@mech.sharif.ir
Shahid Sattari Air University
, Tehran, Iran, 1384674334
Search for other works by this author on:
M. Taeibi-Rahni,
M. Taeibi-Rahni
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334
Search for other works by this author on:
M. Salimi
M. Salimi
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334
Search for other works by this author on:
R. Farhadi-Azar
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334
M. Ramezanizadeh
Department of Aerospace Engineering,
Shahid Sattari Air University
, Tehran, Iran, 1384674334e-mail: ramezanizadeh@mech.sharif.ir
M. Taeibi-Rahni
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334
M. Salimi
Department of Aerospace Engineering,
Sharif University of Technology
, Tehran, Iran, 1384674334J. Fluids Eng. Mar 2011, 133(3): 031202 (13 pages)
Published Online: March 10, 2011
Article history
Received:
January 19, 2010
Revised:
February 3, 2011
Online:
March 10, 2011
Published:
March 10, 2011
Citation
Farhadi-Azar, R., Ramezanizadeh, M., Taeibi-Rahni, M., and Salimi, M. (March 10, 2011). "Compound Triple Jets Film Cooling Improvements via Velocity and Density Ratios: Large Eddy Simulation." ASME. J. Fluids Eng. March 2011; 133(3): 031202. https://doi.org/10.1115/1.4003589
Download citation file:
Get Email Alerts
Related Articles
Correlation of Film-Cooling Effectiveness From Thermographic Measurements at Enginelike Conditions
J. Turbomach (October,2002)
Large Eddy Simulation of Leading Edge Film Cooling—Part II: Heat Transfer and Effect of Blowing Ratio
J. Turbomach (October,2008)
Film Cooling of a Cylindrical Leading Edge With Injection Through Rows of Compound-Angle Holes
J. Heat Transfer (August,2001)
Three Component Velocity Field Measurements in the Stagnation Region of a Film Cooled Turbine Vane
J. Turbomach (July,2002)
Related Chapters
Random Turbulence Excitation in Single-Phase Flow
Flow-Induced Vibration Handbook for Nuclear and Process Equipment
Studies Performed
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential