Calculation of heat transfer rates to gas turbine blades

Calculation of heat transfer rates to gas turbine blades
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燃气轮机叶片传热率的计算

DOI:
10.1016/s0017-9310(81)80010-5
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发表时间:
1981
影响因子:
5.2
通讯作者:
W. B. Browne
W. B. Browne
中科院分区:
工程技术2区
文献类型:
--
作者:
L. D. Daniels;W. B. Browne

文献摘要

被引文献

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本文用五种计算机程序计算了燃气涡轮机叶片的传热率,并与叶栅的实验结果进行了比较。程序使用不同的方法来模拟湍流量。这项实验工作是最近在牛津大学弗里皮斯顿隧道进行的。
Five computer programs are used to calculate heat transfer rates to gas turbine blades and the results compared with experimental work on blade cascades. The programs use different methods to model the turbulence quantities. The experimental work was carried out recently in the University of Oxford freepiston tunnel.