SKIN FRICTION AND HEAT TRANSFER AT AN INFINITE SWEPT ATTACHMENT LINE.

被引：0

作者：

Poll, D.I.A.

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来源：

Aeronautical Quarterly | 1981年 / 32卷 / pt 4期

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D O I：

10.1017/s0001925900009215

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摘要：

Simple, yet reasonably accurate, expressions are developed for the prediction of skin friction and heat transfer coefficient at an infinite swept attachment line using the concepts of 'reference temperature' and 'Reynolds analogy'. The formulas are then used to investigate the effect of varying sweep angle with constant undisturbed free stream conditions in the limits of very low and very high Mach number.

引用

页码：299 / 318

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