Aerodynamic performance effects of leading-edge geometry in gas-turbine blades
Author:
Publisher
Elsevier BV
Subject
Management, Monitoring, Policy and Law,Mechanical Engineering,General Energy,Building and Construction
Reference41 articles.
1. Rotor-blades’ profile influence on a gas-turbine’s compressor effectiveness;Lebele-Alawa;Appl Energy,2008
2. Thermoeconomic impact on combined cycle performance of advanced blade cooling systems;Ghigliazza;Appl Energy,2009
3. Development and multi-utility of an ANN model for an industrial gas turbine;Fast;Appl Energy,2009
4. Axial-flow compressor design optimization. 1. Pitchline analysis and multivariable objective function influence;Massardo;Trans ASME, J Turbomachinery,1990
5. Axial-flow compressor design optimization. 2. Throughflow analysis;Massardo;Trans ASME, J Turbomachinery,1990
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