Abstract

The plane laminar boundary layer equations with a power-law velocity distribution U(x) = cx m at the outer edge admit in the region m < 0 two families of similar solutions [1]. In contrast with the known Falkner-Skan solution [2], the second family of velocity profiles is characterized by reverse flow near the wall. The integral properties of this family of profiles are used widely in approximate methods for calculating the plane boundary layer to describe

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