Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
2. United Technologies—Pratt & Whitney, East Hartford, Connecticut 06108
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36308
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1. Vortical structure in the wake of a transverse jet
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3. Mixing of Multiple Jets With a Confined Subsonic Crossflow: Part II—Opposed Rows of Orifices in Rectangular Ducts
4. Experiments in Dilution Jet Mixing
5. Turbulence Levels are High at the Combustor-Turbine Interface
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2. Cooling characteristics of dilution holes in can-type combustor of micro gas turbine;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2023-05-25
3. Effect of side dilution jets on the velocity field and mixing in swirl and bluff-body stabilised annular confined flows;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2022-07-15
4. Comparison of Finite-Volume and Spectral/hp Methods for Large-Eddy Simulation of Combustor Port Flow;AIAA Journal;2022-07
5. Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes;Journal of Propulsion and Power;2019-01
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