Experimental study on a dual synthetic jets liquid cooling device
Y Kang, Z Xia, Z Luo, X Deng, Y Zhu, C Peng - Applied Energy, 2024 - Elsevier
To address the growing heat dissipation requirements of high heat flux electronic devices,
this work presents experimental research on a dual synthetic jets (DSJ) liquid cooling …
this work presents experimental research on a dual synthetic jets (DSJ) liquid cooling …
[HTML][HTML] Heat transfer enhancement on a concave surface using sweeping impinging jets: Comparison of vortex-based and conventional oscillators
While the impinging sweeping jet generated by a conventional fluidic oscillator has been
extensively investigated for its remarkable convective heat transfer performance, the cooling …
extensively investigated for its remarkable convective heat transfer performance, the cooling …
Convective heat transfer improvement for a single row of continuous air jets by the acoustic-actuator integration
An experimental study is performed to identify the roles of acoustic-actuator integration on
improving convective heat transfer from a row of continuous air jets onto a flat target surface …
improving convective heat transfer from a row of continuous air jets onto a flat target surface …
Numerical investigation on the heat transfer performance of the liquid metal array jet impingement
R Liu, H Zhang, M Nie, L Yao, X Li, F Li - International Journal of Thermal …, 2025 - Elsevier
Liquid metal jet impingement can meet the cooling demands of heat fluxes exceeding 1
MW/m 2. However, there is currently a lack of detailed research on the flow and heat transfer …
MW/m 2. However, there is currently a lack of detailed research on the flow and heat transfer …
Flow structure and heat transfer characteristics of sweeping and steady impingement jets with/without chevrons on a semi-circular concave surface
Striving for improved gas turbine performance requires operating at higher gas flow
temperatures, posing challenges in preserving the structural integrity of the gas turbine. To …
temperatures, posing challenges in preserving the structural integrity of the gas turbine. To …
Large-eddy simulations of the cavitation impact performance in reflux self-excited oscillating nozzles
L Wang, S Fan, Z Fang, X Li, W Wu - Physics of Fluids, 2024 - pubs.aip.org
Existing research on reflux self-excited oscillating nozzles (RSONs) has primarily focused on
flow drag reduction and combustion mixing, with relatively little investigation of their impact …
flow drag reduction and combustion mixing, with relatively little investigation of their impact …
Conjugate heat transfer simulations of a radially cooled gas turbine blade leading edge using a vortex-based fluidic oscillator for sweeping jet impingement
A Farooq, S Chen, Y Zhang, P Yang - Physics of Fluids, 2024 - pubs.aip.org
The turbine blades of aero engines are subjected to extremely high temperatures,
particularly at the leading edge, where temperatures can reach approximately 1800–2000 K …
particularly at the leading edge, where temperatures can reach approximately 1800–2000 K …