Effect of coolant temperature and mass flow on film cooling of turbine blades-Reference-Cited by-同舟云学术

Effect of coolant temperature and mass flow on film cooling of turbine blades

Published:1997-01 Issue:2 Volume:40 Page:435-445
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Garg Vijay K.,Gaugler Raymond E.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference21 articles.

1. Film cooling;Goldstein,1971

2. Heat transfer in film-cooled turbine blades;Garg;ASME paper 93-GT-81,1993

3. Prediction of film cooling on gas turbine airfoils;Garg;ASME paper 94-GT-16,1994

4. Leading edge film cooling effects on turbine blade heat transfer;Garg;ASME paper 95-GT-275,1995

5. Computations of a film cooled turbine rotor blade with non-uniform inlet temperature distribution using a three-dimensional viscous procedure;Weigand;ASME paper 94-GT-15,1994

Cited by 33 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Influence mechanism of impingement and film on the flow and heat transfer of turbine outer ring with composite cooling structure under different operating parameters;Applied Thermal Engineering;2024-06

2. Application of a Ranque–Hilsch Vortex Flow in an Internal Cooling of a Gas Turbine Engine Blade;ASME Open Journal of Engineering;2024-01-01

3. Effect of Porosity and Injection Ratio on the Performance of Transpiration Cooling through Gyroids;International Journal of Turbomachinery, Propulsion and Power;2023-12-01

4. Study on the Milling Machinability of Bamboo-Based Fiber Composites;Forests;2023-09-21

5. Deep‐Learning-Based Uncertainty Analysis of Flat Plate Film Cooling With Application to Gas Turbine;Aerospace Research Communications;2023-03-30