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

被引：0
|
作者：
Poll, D.I.A.
机构：
来源：
Aeronautical Quarterly | 1981年 / 32卷 / pt 4期
关键词：
D O I：
10.1017/s0001925900009215
中图分类号：
学科分类号：
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
收藏
页码：299 / 318
相关论文
共 50 条
12345