Thermal stress analysis of the FGLCS in hypersonic vehicles: Their application to fuel injection struts in scramjets-Reference-Cited by-同舟云学术

Thermal stress analysis of the FGLCS in hypersonic vehicles: Their application to fuel injection struts in scramjets

Published:2017-08 Issue: Volume:99 Page:157-165
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Xie Weihua,Peng Zujun,Meng Songhe,Xu Chenghai,Yi Fajun,Jin Hua,Du Shanyi

Funder

National Natural Science Foundation of China

National Basic Research Program of China

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference22 articles.

1. Evaluation of kerosene fuelled scramjet combustor using a combination of cooled and uncooled struts;Chandrasekhar;Def Sci J,2014

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

3. Effect of structural factors on maximum aerodynamic heat flux of strut leading surface;Bao;Appl Therm Eng,2014

4. Experimental investigations of hydrocarbon fueled scramjet combustor by employing high temperature materials for the construction of fuel injection struts;Chandrasekhar;Int J Sci Tech,2012

5. Oxidation behavior of oxidation protective coatings for PIP–C/SiC composites at 1500°C;Xiang;Ceram Int,2012

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Failure tolerant functionally graded fiber-reinforced UHTCs exposed to hypersonic flows;Composites Part A: Applied Science and Manufacturing;2024-10

2. Transpiration cooling performances of oriented porous structures with lateral permeability under local block conditions;Applied Thermal Engineering;2024-04

3. Elevated temperature tensile and bending strength of ultra-high temperature ceramic matrix composites obtained by different processes;Journal of the European Ceramic Society;2023-09

4. Fluid-thermo-structural response of actively cooled scramjet combustor in hypersonic accelerating-cruise flight;International Journal of Heat and Mass Transfer;2022-09

5. Numerical Study of the Influence of Coupling Interface Emissivity on Aerogel Metal Thermal Protection Performance;Gels;2021-12-03