Discrete-jet film cooling: a comparison of computational results with experiments

JH Leylek, RD Zerkle - 1994 - asmedigitalcollection.asme.org
Large-scale computational analyses have been conducted and results compared with
experiments to understand coolant jet and crossflow interaction in discrete-jet film cooling …

Convective heat transfer and aerodynamics in axial flow turbines

MG Dunn - Turbo Expo: Power for Land, Sea, and …, 2001 - asmedigitalcollection.asme.org
The primary focus of this paper is convective heat transfer in axial flow turbines. Research
activity involving heat transfer generally separates into two related areas: predictions and …

Progress towards understanding and predicting heat transfer in the turbine gas path

RJ Simoneau, FF Simon - International journal of heat and fluid flow, 1993 - Elsevier
A new era is dawning in the ability to predict convection heat transfer in the turbine gas path.
We feel that the technical community now has the capability to mount a major assault on this …

Impact of rotor–stator interaction on turbine blade film cooling

RS Abhari - 1996 - asmedigitalcollection.asme.org
The goal of this study is to quantify the impact of rotor–stator interaction on surface heat
transfer of film cooled turbine blades. In Section I, a steady-state injection model of the film …

Thermal-electric finite element analysis and experimental validation of bipolar electrosurgical cautery

RE Dodde, SF Miller, JD Geiger, AJ Shih - 2008 - asmedigitalcollection.asme.org
Cautery is a process to coagulate tissues and seal blood vessels using heat. In this study,
finite element modeling (FEM) was performed to analyze temperature distribution in …

Modeling of film cooling—part II: model for use in three-dimensional computational fluid dynamics

A Burdet, RS Abhari, MG Rose - 2007 - asmedigitalcollection.asme.org
Computational fluid dynamics (CFD) has recently been used for the simulation of the
aerothermodynamics of film cooling. The direct calculation of a single cooling hole requires …

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

VK Garg, RE Gaugler - 1997 - asmedigitalcollection.asme.org
An existing three-dimensional Navier–Stokes code (Arnone et al., 1991), modified to include
film cooling considerations (Garg and Gaugler, 1994), has been used to study the effect of …

Heat transfer on a film-cooled rotating blade using different turbulence models

VK Garg - International Journal of Heat and Mass Transfer, 1999 - Elsevier
A three-dimensional Navier–Stokes code has been used to compute the heat transfer
coefficient on a film-cooled, rotating turbine blade. The blade chosen is the ACE rotor with …

Aerodynamic and Heat Flux Measurements in a Single-Stage Fully Cooled Turbine—Part I: Experimental Approach

CW Haldeman, RM Mathison, MG Dunn… - 2008 - asmedigitalcollection.asme.org
This paper describes the experimental approach utilized to perform experiments using a
fully cooled rotating turbine stage to obtain film effectiveness measurements. Significant …

Comparison of predicted and experimental Nusselt number for a film-cooled rotating blade

VK Garg, RS Abhari - International journal of heat and fluid flow, 1997 - Elsevier
The predictions from a three-dimensional (3-D) Navier-Stokes code have been compared to
the Nusselt number data obtained on a film-cooled, rotating turbine blade. The blade chosen …