Investigation of Cooling Effectiveness of Gas Turbine Inlet Fogging Location Relative to the Silencer

Journal of Engineering for Gas Turbines and Power - United States
doi 10.1115/1.4004044
Full Text
Abstract

Available in full text

Date
Authors
Publisher

ASME International

Related search

Analysis of Gas Turbine Performance With Inlet Air Cooling Techniques Applied to Brazilian Sites

Journal of Aerospace Technology and Management
Aerospace Engineering
2012English

Application of Inlet Fogger Cooling System for Economical Power Boosting of Gas Turbine

TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
2013English

Inlet Fogging of Gas Turbine Engines: Part B — Fog Droplet Sizing Analysis, Nozzle Types, Measurement and Testing

2002English

Comparative and Exergetic Study of a Gas Turbine System With Inlet Air Cooling

Tehnicki Vjesnik
Engineering
2018English

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation

2016English

Thermionic Method of Cooling Turbine Blades of Spacecraft Gas Turbine Converters

Engineering Journal: Science and Innovation
2016English

Weight Reduction in a Marine Gas Turbine Inlet

1985English

Field Experience With Gas Turbine Inlet Air Filtration

1981English

Performance of Gas Turbine Film Cooling With Backward Injection

Energy and Power Engineering
2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy