Review of jet impingement cooling of electronic devices: Emerging role of surface engineering

S Sarkar, R Gupta, T Roy, R Ganguly… - International Journal of …, 2023 - Elsevier
The rising requirements of computing capability with an ever-declining packaging volume
has triggered a global surge in the thermal management industry of electronic devices over …

A modern review on jet impingement heat transfer methods

SV Ekkad, P Singh - Journal of Heat Transfer, 2021 - asmedigitalcollection.asme.org
Jet impingement cooling is considered as one of the most effective heat transfer
enhancement techniques. The primary mode of heat transfer enhancement is due to the flow …

Energy saving in thermal energy systems using dimpled surface technology–A review on mechanisms and applications

S Rashidi, F Hormozi, B Sundén, O Mahian - Applied Energy, 2019 - Elsevier
Recently, dimpled surfaces have found great attention due to their abilities in energy
management and heat transfer enhancement, low weight, small values of pressure drop …

Convection from multiple air jet impingement-A review

FV Barbosa, SFCF Teixeira, JCF Teixeira - Applied Thermal Engineering, 2023 - Elsevier
Multiple jet impingement is widely implemented in several industrial processes. The efficacy
of this convective process depends on various parameters from the geometrical variables of …

[HTML][HTML] A review of recent studies on rotating internal cooling for gas turbine blades

K Yeranee, RAO Yu - Chinese Journal of Aeronautics, 2021 - Elsevier
Gas turbines have been used extensively for aircraft and marine propulsions as well as land-
based power generation because of their high thermal efficiency and large power to weight …

Experimental and numerical investigation of unsteady impingement cooling within a blade leading edge passage

L Yang, J Ren, H Jiang, P Ligrani - International Journal of Heat and Mass …, 2014 - Elsevier
The cooling passage within the leading edge of a turbine blade is simulated using a
cylindrical target channel supplied by 10 impinging jets, with exit flow in the axial direction …

Experimental and numerical study of swirl impingement cooling for turbine blade leading edge with internal ridged wall and film extraction holes

Y Luan, Y Rao, H Yan - International Journal of Heat and Mass Transfer, 2023 - Elsevier
This paper presents a comparative experimental and numerical study of the internal heat
transfer and pressure loss of swirl impingement cooling for turbine blade leading edge with …

Numerical research of a new vortex double wall cooling configuration for gas turbine blade leading edge

X Fan - International Journal of Heat and Mass Transfer, 2022 - Elsevier
In order to explore new cooling methods to further improve the cooling performance for the
gas turbine blade leading edge, a vortex double wall cooling configuration is established …

Numerical study on flow and heat transfer characteristics of swirling jet on a dimpled surface with effusion holes at turbine blade leading edge

D Kong, C Zhang, Z Ma, C Liu, SA Isaev, T Guo… - Applied Thermal …, 2022 - Elsevier
In this paper, a numerical study has been conducted on the effect of the offset of jet holes on
the flow structure and heat transfer of swirling flow in a concave target chamber with various …

Progress of porous/lattice structures applied in thermal management technology of aerospace applications

J Liu, M Xu, R Zhang, X Zhang, W Xi - Aerospace, 2022 - mdpi.com
With lightweight, multifunctional, and designable characteristics, porous/lattice structures
have started to be used in aerospace applications. Porous/lattice structures applied in the …