Gas turbine vane film cooling for engine-realistic combustor flows

<p>While all lean-burn combustors follow the same design principles and intent, there exist a wide variety of combustor geometries in use, whose downstream aerothermal fields are unquantified. Conventional design processes for the nozzle guide vane (NGV) range from simple ones that use homogen...

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Bibliographic Details
Main Author: Saw, JJH
Other Authors: Rosic, B
Format: Thesis
Language:English
Published: 2023
Subjects: