Affiliation:
1. Gas Turbine Laboratory, M.I.T., Cambridge, Mass.
Abstract
Rotational and three-dimensional terms are added to a strip-integral method for predicting the behavior of turbulent boundary layers. The secondary flow in the boundary layers is analyzed, and a theory for the momentum transport in the corner regions is used to couple the development of all the boundary layers. Simple assumptions for the potential flow and wake regions complete a model which allows the calculation of the whole channel flow, with only the specification of the inlet boundary layers.
Cited by
13 articles.
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