Research progress of transpiration cooling for aircraft thermal protection

Q Mi, SH Yi, DD Gang, XG Lu, XL Liu - Applied Thermal Engineering, 2024 - Elsevier
The challenge of aerodynamic heating in hypersonic vehicles becomes more significant as
they reach higher Mach numbers, which poses a major obstacle in aircraft design. The …

Research progress on active thermal protection for hypersonic vehicles

S Zhang, X Li, J Zuo, J Qin, K Cheng, Y Feng… - Progress in Aerospace …, 2020 - Elsevier
Hypersonic vehicles with scramjet engine as propulsion devices is one of the most important
developing trends in the aerospace field for both commercial and military application. The …

[HTML][HTML] Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles

ZHU Yinhai, P Wei, XU Ruina, P Jiang - Chinese Journal of Aeronautics, 2018 - Elsevier
Hypersonic vehicles with turbojet, ramjet, and scramjet engines are expected to be widely
applied to future transportation systems. Due to high-speed flight in the atmosphere, body …

Investigations on porous media customized by triply periodic minimal surface: Heat transfer correlations and strength performance

Z Cheng, X Li, R Xu, P Jiang - … Communications in Heat and Mass Transfer, 2021 - Elsevier
Porous media are used widely in technological (eg, transpiration cooling and heat sinks for
electronic devices), and biological (eg, bone tissue) applications. The requirement for …

Research progress on strut-equipped supersonic combustors for scramjet application

J Chang, J Zhang, W Bao, D Yu - Progress in Aerospace Sciences, 2018 - Elsevier
Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …

Transpiration cooling with phase change by functionally graded porous media

Z Cheng, R Xu, P Jiang - International Journal of Heat and Mass Transfer, 2023 - Elsevier
Transpiration cooling using liquid coolants is considered one of the most promising thermal
protection techniques for new generation aerospace vehicles. The leading edges are …

Transpiration cooling for additive manufactured porous plates with partition walls

G Huang, Z Min, L Yang, PX Jiang, M Chyu - International Journal of Heat …, 2018 - Elsevier
Transpiration cooling is an effective method to protect high heat flux surfaces such as rocket
combustion chambers. However, this technology is currently not applicable for turbine …

Experimental investigation on additively manufactured transpiration and film cooling structures

Z Min, G Huang, SN Parbat… - Journal of …, 2019 - asmedigitalcollection.asme.org
The last 50 years has witnessed significant improvement in film cooling technologies while
transpiration cooling is still not implemented in turbine airfoil cooling. Although transpiration …

Experimental investigation of effusion and transpiration air cooling for single turbine blade

M Kim, DH Shin, JS Kim, BJ Lee, J Lee - Applied Thermal Engineering, 2021 - Elsevier
A great number of studies have been conducted on a film cooling for turbine blades, which is
to prevent thermal damage on blades originated from high turbine inlet temperature …

Experimental study on transpiration cooling with phase change in rotating detonation engine

S Lu, Q Zhu, J Gong, H Chen, H Ying - Applied Thermal Engineering, 2025 - Elsevier
Transpiration cooling with phase change is an effective method for protecting high heat flux
walls from ablation in combustion chambers and spaceflight vehicles. The combustion …