Conjugate heat transfer and flow analysis on double-wall cooling with impingement induced swirling and film cooling

J Zhang, Q Zheng, J Xu, G Yue, Y Jiang - Applied Thermal Engineering, 2023 - Elsevier
A novel double-wall cooling configuration with impingement induced swirling film cooling is
investigated in present paper. The effects of impingement inclined angle, blowing ratio, film …

Experimental investigation of full-coverage film cooling characteristic of single/double-wall cooling vane

J Zhang, C Liu, W Xu, L Zhang - Thermal Science and Engineering …, 2024 - Elsevier
This paper employed the pressure sensitive paint (PSP) technique to measure the adiabatic
film cooling effectiveness distributions of both the single-wall cooling vane (SCV) and the …

Experimental study of impingement Effusion-Cooled Double-Wall combustor liners: thermal analysis

T Jackowski, M Elfner, HJ Bauer - Energies, 2021 - mdpi.com
A new experimental study is presented for a combustor with a double-wall cooling design.
The inner wall at the hot gas side features effusion cooling with 7-7-7 laidback fan-shaped …

Flow and heat transfer analysis on impingement/effusion cooling configuration including jet orifices with conformal pins

C Chen, Y Jiang, X Lao, Y Chen, L Dong - Physics of Fluids, 2024 - pubs.aip.org
An improving impingement/effusion cooling configuration including jet orifices with
conformal pins is investigated by computational fluid dynamics numerical simulation. Two …

Propulsion Research and Academic Programs at the University of Alabama in Huntsville–Research Review

RA Frederick, L Thomas, PM Ligrani - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
The Propulsion Research Center (PRC) is in its 33rd year at the University of Alabama in
Huntsville (UAH). The mission of the Propulsion Research Center is to provide an …

Experimental Study of Impingement Effusion Cooled Double-Wall Combustor Liners: Aerodynamic Analysis with Stereo-PIV

T Jackowski, M Elfner, HJ Bauer, K Stichling, M Hahn - Energies, 2021 - mdpi.com
A new experimental study is presented for a combustor with a double-wall cooling design.
The inner wall at the hot gas side features effusion cooling with 7-7-7 laidback fan-shaped …

[HTML][HTML] Unique Coolant Supply Passage Arrangements to Induce Large-Scale Vortex within Turbine Blade Interior Leading Edge Chambers

Y Cai, X Liu, Y Sun, X Fan, J Wang - Energies, 2024 - mdpi.com
Gas turbines are widely applied in many fields, and blade cooling is a key way to improve
gas turbines' power and efficiency. In order to explore a high-efficiency cooling method, a …

Propulsion Research and Academic Programs at the University of Alabama in Huntsville-30th Anniversary Summary

RA Frederick, L Thomas, PM Ligrani - AIAA Propulsion and Energy …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3347. vid The UAH Propulsion
Research Center (PRC) is in its 30th year at the University of Alabama in Huntsville (UAH) …

Exploration of a Variation of Double-Wall Vortex Cooling Structure for Advanced Gas Turbine Blade Cooling

X Fan, X Liu - Available at SSRN 4196875 - papers.ssrn.com
As a series study of double-wall vortex cooling mothod for the gas turbine blade leading
edge, a new variant configuration was proposed and explored using numerical simulation …