International Journal of Turbomachinery, Propulsion and Power (Dec 2023)

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

  • Benjamin J. Brimacombe,
  • James A. Scobie,
  • Joseph M. Flynn,
  • Carl M. Sangan,
  • Oliver J. Pountney

DOI
https://doi.org/10.3390/ijtpp8040050
Journal volume & issue
Vol. 8, no. 4
p. 50

Abstract

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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.

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