Abstract
Computational investigations are reported on the local flow and heat transfer characteristics from staggered, multiple circular air jets impinging on a flat surface with effusion holes. The geometrical and flow parameters for the computational study are chosen as per the experimental arrangement of Cho and Rhee J Turbomachinery 123:601–608, (14) so as to explain salient features observed in these experiments. The two peaks in the Nusselt number observed in the case of H/D = 6 and three peaks in the case of H/D = 2 are attributed to the flow characteristics such as primary vortices forming an up-wash region, followed by secondary vortices resulting in a secondary stagnation zone. The magnitude of local peak in heat transfer increases up to 88% with increasing values of D/d from 0.5 to 1.5 at Re = 10,000.
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Abbreviations
- c:
-
Center to center distance of jet holes, m
- D:
-
Diameter of jet hole, m
- d:
-
Diameter of film hole, m
- H:
-
Distance between target surface and jet hole exit, m
- kf :
-
Thermal conductivity of fluid, W/m–K
- m:
-
Mass flow rate, kg/sec
- Nu:
-
Nusselt number
- q″:
-
Local heat flux, W/m2
- p:
-
Local static pressure, N/m2
- pmax :
-
Maximum local static pressure, N/m2
- Cp :
-
Pressure coefficient (p/p max)
- p0 :
-
Stagnation pressure, N/m2
- Tj :
-
Jet temperature, K
- Ttp :
-
Target plate temperature, K
- v:
-
Velocity magnitude in y—direction, m/s
- U:
-
Jet exit velocity, m/s
- t1 :
-
Jet plate thickness, m
- t2 :
-
Target plate thickness, m
- x:
-
x-co-ordinate, m
- y:
-
y-co-ordinate, m
- z:
-
z-co-ordinate, m
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Ashok kumar, M., Prasad, B.V.S.S.S. Computational flow and heat transfer of multiple circular jets impinging on a flat surface with effusion. Heat Mass Transfer 47, 1121–1132 (2011). https://doi.org/10.1007/s00231-011-0776-x
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DOI: https://doi.org/10.1007/s00231-011-0776-x