Numerical investigation on a double layer combined cooling structure for aerodynamic heat control of hypersonic vehicle leading edge-Reference-Cited by-同舟云学术

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Numerical investigation on a double layer combined cooling structure for aerodynamic heat control of hypersonic vehicle leading edge

Published:2020-03 Issue: Volume:169 Page:114949
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Ding Rui,Wang Jianhua,He Fei,Wang Meng,Luan Yun,Dong Guangqi,Tang Longsheng

Funder

University of Science and Technology of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference36 articles.

1. D.E. Glass, Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles, in: 15th AIAA Space Planes and Hypersonic Systems and Technologies Conference, 2008, pp. 1–36.

2. Power from space;Lior;Energy Convers. Manage.,2001

3. An experimental investigation on transpiration cooling performances using solid hydrogel as coolant;Qian;Appl. Therm. Eng.,2019

4. Self-pumping transpiration cooling with a protective porous armor;Huang;Appl. Therm. Eng.,2020

5. Numerical investigation on the optimization of local transpiration cooling effectiveness;Shen;Appl. Therm. Eng.,2017

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