Comparison of predicted and experimental Nusselt number for a film-cooled rotating blade
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference32 articles.
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4. Comparison of time-resolved measurements and numerical calculations;Abhari;J. Turbomachinery,1992
5. Comparison of different two-equation turbulence models for prediction of film cooling from two rows of holes;Amer;Numer. Heat Transfer,1992
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1. Effect of RANS-Type Turbulence Models on Adiabatic Film Cooling Effectiveness over a Scaled Up Gas Turbine Blade Leading Edge Surface;Journal of The Institution of Engineers (India): Series C;2016-06-23
2. Computation of leading edge film cooling from a CONSOLE geometry (CONverging Slot hOLE);Thermophysics and Aeromechanics;2016-01
3. Numerical Modeling of Heat Transfer and Flow Phenomena in an Axial Rotating Rotor Cascade;Numerical Heat Transfer, Part A: Applications;2015-02-12
4. Numerical investigation of heat transfer coefficient in a low speed 1.5-stage turbine;Journal of Thermal Science;2014-07-18
5. Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine;Journal of Turbomachinery;2013-12-04
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