3D Investigations of Nozzle Cluster Platform Cooling in the Variant with Doubled V-Shaped Dimplesand Hemispherical Protrusions between Them and in the Variant with Ribs when the Platform Is Blowing off through the Holes in the Shield

By results of 3D calculations carried out, the computational study was fulfilled for the local and averaged heat transfer coefficients, hydrodynamic characteristics of platform cooling channels with meridional compression in the cavity between the shield and the platform for the variant with doubled V-shaped dimples with hemispherical protrusions between them as well as for the variant with ribs on the platform surface blown down through the holes in the shield over the platform. Investigations of the platform cooling efficiency for these variants are carried out.

Authors

Publication Details

Journal
Russian Aeronautics
Published
2024-12-01
DOI
https://doi.org/10.3103/s1068799824040159
Primary Topic
Heat transfer and supercritical fluids
Type
article
Field-Weighted Citation Impact
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article

3D Investigations of Nozzle Cluster Platform Cooling in the Variant with Doubled V-Shaped Dimplesand Hemispherical Protrusions between Them and in the Variant with Ribs when the Platform Is Blowing off through the Holes in the Shield

Yu. G. Gorelov
Russian Aeronautics
Heat transfer and supercritical fluids
article

3D Investigations of Nozzle Cluster Platform Cooling in the Variant with Doubled V-Shaped Dimplesand Hemispherical Protrusions between Them and in the Variant with Ribs when the Platform Is Blowing off through the Holes in the Shield

Yu. G. Gorelov
article en

Abstract

By results of 3D calculations carried out, the computational study was fulfilled for the local and averaged heat transfer coefficients, hydrodynamic characteristics of platform cooling channels with meridional compression in the cavity between the shield and the platform for the variant with doubled V-shaped dimples with hemispherical protrusions between them as well as for the variant with ribs on the platform surface blown down through the holes in the shield over the platform. Investigations of the platform cooling efficiency for these variants are carried out.

Russian AeronauticsVol. 67(4)
Openalex Percentile: Top 71%
Heat transfer and supercritical fluids
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