CALCULATION OF TURBULENT BOUNDARY LAYERS ON ROUGH SURFACES IN PRESSURE GRADIENT

被引:102
作者
DVORAK, FA
机构
关键词
D O I
10.2514/3.5386
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Rough surface skin-friction relations previously described in the literature are expanded in scope and range of applicability. The resulting equat%ions are combined with the momentum integral equation and an auxiliary equation for the shape factor to provide a calculation method for predicting the growth of the turbulent boundary layer over a rough surface in pressure gradient. Several comparisons have been made between the calculation method and available experimental data in zero, favorable, and adverse pressure gradients. The agreement in g%eneral is good.
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页码:1752 / &
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