Development of High Performance Film Cooling of 1700 Degree C Class Gas Turbines

Journal of High Temperature Society
doi 10.7791/jhts.33.264
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Sumart Processing Society for Minerals, Environment and Energy

Related search

An Advanced Impingement/Film Cooling Scheme for Gas Turbines – Numerical Study

International Journal of Numerical Methods for Heat and Fluid Flow
Mechanics of MaterialsApplied MathematicsComputer Science ApplicationsMechanical Engineering
2006English

Performance of Gas Turbine Film Cooling With Backward Injection

Energy and Power Engineering
2013English

Environmental Performance of Industrial Gas Turbines

1974English

Superalloy Development for Aircraft Gas Turbines

1969English

Effect of Hole Configurations on Film Cooling Performance

Numerical Heat Transfer; Part A: Applications
Numerical AnalysisCondensed Matter Physics
2019English

High Temperature Sensors for Gas Turbines

1969English

A Study of Cycle Performance of Ceramic Gas Turbines

1997English

The Design of High-Efficiency Turbomachinery and Gas Turbines

2014English

Towards the Development of the Finger-Top Gas Turbines

The proceedings of the JSME annual meeting
2003English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy