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Effect of Porosity and Injection Ratio on the Performance of Transpiration Cooling through Gyroids †.

Authors :
Brimacombe, Benjamin J.
Scobie, James A.
Flynn, Joseph M.
Sangan, Carl M.
Pountney, Oliver J.
Source :
International Journal of Turbomachinery, Propulsion & Power; Dec2023, Vol. 8 Issue 4, p50, 12p
Publication Year :
2023

Abstract

This paper presents experimental measurements of adiabatic effectiveness for three transpiration cooling porosities ( ϕ = 0.3, 0.4, and 0.5) constructed from gyroid lattice structures. To the authors' knowledge, this is the first use of a Triply Periodic Minimal Surface (TPMS) function to produce transpiration test coupons of varying porosity. Polymer gyroid lattice structures were successfully printed using Stereolithography (SLA) down to ϕ = 0.3 for a print resolution of 25 microns and unit cell size of 2 mm. Cooling performance was measured in a small-scale wind tunnel. High-resolution Infrared Thermography was used to determine wall temperatures downstream of the porous section. When tested at both common blowing ratios ( M = 0.029, 0.048, and 0.062) and common injection ratios ( F   = 0.010, 0.017, and 0.022) the cooling performance was found to be dependent on porosity for constant M but not for constant F . Having determined F as the more important parameter for comparison, results are presented alongside transpiration and effusion data from literature. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
2504186X
Volume :
8
Issue :
4
Database :
Complementary Index
Journal :
International Journal of Turbomachinery, Propulsion & Power
Publication Type :
Academic Journal
Accession number :
174440719
Full Text :
https://doi.org/10.3390/ijtpp8040050