An Introduction to the Calculus of Finite Differences and Difference Equations
An Introduction to the Calculus of Finite Differences and Difference Equations
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有限差分和差分方程微积分简介
DOI:
10.2307/2282311
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发表时间:
1960
期刊:
影响因子:
2.7
通讯作者:
K. Miller
中科院分区:
文献类型:
--
作者:
K. Miller
A stator aerofoil blade for a gas turbine engine is manufactured in the form of a heat pipe so that during engine operation, the blade remains substantially isothermal. Localized thermal gradients within the blade are minimized thereby reducing the possibility of blade distortion or cracking. A shroud ring for a gas turbine engine is manufactured in the form of a heat pipe so that during engine operation, the ring remains substantially isothermal. Localized thermal gradients within the ring are minimized, thereby reducing the possibility of ring distortion occurring.