Improved film cooling from cylindrical angled holes with triangular tabs: effect of tab orientations
Authors:
- Hasan NasirHNHasan Nasir
- Sumanta AcharyaSASumanta Acharya
- Srinath EkkadSESrinath Ekkad
- 1 October 2003
- journal article
- Published by Elsevier in International Journal of Heat and Fluid Flow
- Vol. 24 (5) , 657-668
Abstract
No abstract availableKeywords
This publication has 19 references indexed in Scilit:
- Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded ExitsJournal of Turbomachinery, 1998
- Heat Transfer Coefficient Measurements of Film-Cooling Holes With Expanded Exits1998
- Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image MethodJournal of Turbomachinery, 1997
- Heat Transfer Coefficients Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image MethodJournal of Turbomachinery, 1997
- Film-Cooling From Holes With Compound Angle Orientations: Part 2—Results Downstream of a Single Row of Holes With 6d Spanwise SpacingJournal of Heat Transfer, 1994
- Film-Cooling From Holes With Compound Angle Orientations: Part 1—Results Downstream of Two Staggered Rows of Holes With 3d Spanwise SpacingJournal of Heat Transfer, 1994
- Effects of Cooling Films on the Heat Transfer Coefficient on a Flat Plate With Zero Mainstream Pressure GradientJournal of Engineering for Gas Turbines and Power, 1985
- Mass Transfer in the Neighborhood of Jets Entering a CrossflowJournal of Heat Transfer, 1982
- The distortion of a jet by tabsJournal of Fluid Mechanics, 1975
- Heat Transfer and Film Cooling Following Injection Through Inclined Circular TubesJournal of Heat Transfer, 1974