Failure analysis of first stage nozzle in a heavy-duty gas turbine
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Materials Science
Reference31 articles.
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3. Structural Integrity of Turbine Stator Blades Using Different Super Alloys with Internal Cooling at Fluid Temperature Range of 600 K – 700 K;Acta Technica Jaurinensis;2023-11-27
4. A critical review on gas turbine cooling performance and failure analysis of turbine blades;International Journal of Thermofluids;2023-05
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