Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins
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Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins
Thermal Power GenerationIssue 9, (2016)
作者机构:
沈阳航空航天大学辽宁省航空推进系统先进测试技术重点实验室,辽宁,沈阳,110136
作者简介:
基金信息:
DOI:
CLC:V231.1
Published Online:25 September 2016,
Published:2016
稿件说明:
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LI Guangchao, ZHANG Zhandong, ZHANG Wei, et al. Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins[J]. Thermal power generation, 2016, (9).
DOI:
LI Guangchao, ZHANG Zhandong, ZHANG Wei, et al. Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins[J]. Thermal power generation, 2016, (9).DOI:
Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins
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