Variable N-factor method for transition prediction in three-dimensional boundary layers

被引:56
作者
Crouch, JD [1 ]
Ng, LL [1 ]
机构
[1] Boeing Co, Seattle, WA 98124 USA
关键词
D O I
10.2514/2.973
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Linear amplitude methods are presented for estimating the location of transition caused by crossflow instabilities, intended for moderate- to low-turbulence environments. A linear amplitude-based method combines receptivity, linear growth, and an amplitude correlation for predicting transition. Information about the model surface finish (and/or suction distribution) and the freestream disturbance environment is accounted for through the receptivity process. The variable N-factor method is presented as a limiting case, following simplifying assumptions about the receptivity. Transition N factors are presented as a function of the surface roughness. Results show a very good correlation between the variable N-factor method and experimental data.
引用
收藏
页码:211 / 216
页数:6
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