Numerical simulations are carried out aimed at finding a key flow structure which leads to a laminar-turbulent transition of a boundary layer with streaky structures. In the preliminary computation, an array of cuboids is used to form streaky structures inside a boundary layer. Then, a disturbance is introduced into the boundary layer by ejecting a short-duration jet from a hole in the wall into a
Turbulent separation criteria are the most useful since most pressure recovery is done using turbulent boundary layers. There are many criteria that are used. Minimum C p The simplest criterion is that used to estimate when the flow will separate from the leading edge of an airfoil. This rule of thumb states that there is a minimum value of C p that can be tolerated. Numbers such as -10 to -13 are
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