NASA NTRS · 19760027372
An integral method for unsteady laminar boundary layers
Abstract
The Method of Integral Relations is extended to apply to the calculation of Unsteady Flow in a Laminar Boundary Layer. The effectiveness of the method is demonstrated in an application to uniform flow past a circular cylinder, resulting from an impulsive start. Both first and second approximations are worked out, the latter showing good agreement with results of previous calculations.
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Holt, M., Chan, W.-K.. 1975-01-01. An integral method for unsteady laminar boundary layers. https://ntrs.nasa.gov/citations/19760027372
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