Adiabatic Effectiveness and Heat Transfer Coefficient of Shaped Film Cooling Holes on a Scaled Guide Vane Pressure Side Model
Main Authors: | Jan Dittmar, Achmed Schulz, Sigmar Wittig |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2004-01-01
|
Series: | International Journal of Rotating Machinery |
Online Access: | http://dx.doi.org/10.1155/S1023621X04000351 |
Similar Items
-
Adiabatic Effectiveness and Heat Transfer Coefficient of Shaped Film Cooling Holes on a Scaled Guide Vane Pressure Side Model
by: Dittmar Jan, et al.
Published: (2004-01-01) -
Discharge coefficients of nozzle guide vane film cooling holes
by: Rowbury, David
Published: (1998) -
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements for an Internal Turbine Vane Cooling Feature
by: Prausa, Jeffrey Nathaniel
Published: (2017) -
Effect of Blockage Inside Holes on Film Cooling Performance on the Suction Side of a Turbine Guide Vane
by: Li, G., et al.
Published: (2022) -
Effects on Heat Transfer Coefficient and Adiabatic Effectiveness in Combined Backside and Film Cooling with Short-Hole Geometry
by: La Rosa Rivero, Renzo Josue
Published: (2020)