Large eddy simulation of pulsating film cooling on turbine vane
Author:
Funder
Hunan Provincial Natural Science Foundation
National Major Science and Technology Projects of China
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference35 articles.
1. Study on full-coverage film cooling characteristics on turbine vanes under the effect of trailing-edge shock wave;Wang;Int. Commun. Heat Mass Transfer,2023
2. Combustion and emission characteristics of a novel staged combustor for aero gas turbine engine;Li;Aerosp. Sci. Technol.,2023
3. Experimental investigations into the effusion plate wall temperature of impingement/effusion cooling systems for gas turbine combustors;Bai;Aerosp. Sci. Technol.,2023
4. Numerical investigations of the nozzle performance for a rocket-based rotating detonation engine with film cooling;Li;Aerosp. Sci. Technol.,2023
5. Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor;Tian;Aerosp. Sci. Technol.,2022
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