Optimization of gas turbine combustor performance throughout the duty cycle-Reference-Cited by-同舟云学术

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Optimization of gas turbine combustor performance throughout the duty cycle

Published:1996 Issue:2 Volume:26 Page:2819-2825
ISSN:0082-0784
Container-title:Symposium (International) on Combustion
language:en
Short-container-title:Symposium (International) on Combustion

Author:

Davis N.T.,Samuelsen G.S.

Publisher

Elsevier BV

Reference12 articles.

1. Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System

2. Twenty-Third Symposium (International) on Combustion;Brouwer,1990

3. Twenty-Fifth Symposium (International) on Combustion;Padmanabhan,1994

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3. Multiple-objective Optimization of a Subsonic Small-scale Cavity-stabilized Combustor;AIAA Scitech 2019 Forum;2019-01-06

4. Automated Design Optimization of a Small-Scale High-Swirl Cavity-Stabilized Combustor;Journal of Engineering for Gas Turbines and Power;2018-11-29

5. A theoretical and experimental study on flow characterisation in an acoustically excited chamber;Wave Motion;2015-11

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