Vortex-Enhanced Heat Transfer in Turbulent Flow over a Plate with Transverse, V- and Λ-Shaped Single Grooves of Equal Length
Numerical simulations of turbulent separated air flow and heat transfer over a thermally insulated plate containing single V-shaped grooves with hemispherical ends and opening angles of 95°, 180°, and 275° on an isothermal rectangular insert were performed by solving the Reynolds-averaged Navier–Stokes and energy equations using multiblock computational techniques. The closure of the momentum equations employed the differential equations of the SST shear stress transport model. The results revealed a fundamental difference in the mechanisms that enhance separated flow and heat transfer in the grooves, associated with the formation of a U-shaped vortex at the bend of the V-groove and two tornado-like vortices at the upstream-facing ends of the Λ-shaped groove. A localized static pressure drop of about 0.3 between the external flow stagnation regions and low-pressure zones accelerated both the recirculating and secondary swirling flows. The total relative heat transfer from the rectangular section bounding the contour of the V-groove increased by nearly 30% compared to a flat plate, whereas for a transverse groove, the corresponding value reached 1.12.
Authors
- A. Yu. Chulyunin (ORCID: https://orcid.org/0000-0003-3098-5069)
- Д. В. Никущенко (ORCID: https://orcid.org/0000-0001-8549-772X)
- S. A. Isaev (ORCID: https://orcid.org/0000-0003-1763-0693)
- O. O. Mil’man (ORCID: https://orcid.org/0000-0002-7436-0637)
- Elena Nikushchenko (ORCID: https://orcid.org/0000-0003-4955-2693)
Institutions
- Lomonosov Moscow State University (RU)
- State Marine Technical University of St. Petersburg (RU)
- Kaluga State University named after K.E.Tsiolkovski (RU)
- Saint Petersburg State University of Civil Aviation (RU)
Publication Details
- Journal
- Fluid Dynamics
- Published
- 2025-12-01
- DOI
- https://doi.org/10.1134/s0015462825603201
- Primary Topic
- Heat Transfer Mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 0.00