Numerical simulation and structural optimization of transpiration cooling with gradient porous matrix in supersonic condition

Author:

Liu Taolue,Liu Yifei,Ding Rui,Zhu Junqiang,He Fei,Wang Jianhua

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

Elsevier BV

Reference35 articles.

1. Research progress on active thermal protection for hypersonic vehicles;Zhang;Prog. Aero. Sci.,2020

2. Thermal protection systems for space vehicles: a review on technology development, current challenges and future prospects;Nyanna;Acta Astronaut.,2020

3. Q. Mi, S.H. Yi, D. D. Gang, et al. Research progress of transpiration cooling for aircraft thermal protection, Appl. Therm. Eng.. S1359-4311(23)01389-3.

4. Experimental and numerical investigation of micro-scale effusion and transpiration air cooling on cascaded turbine blades;Kim;Case Stud. Therm. Eng.,2022

5. Investigation of transpiration cooling for sintered metal porous struts in supersonic flow;Huang;Appl. Therm. Eng.,2014

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