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An integral method for unsteady laminar boundary layersThe 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.
Document ID
19760027372
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Holt, M.
(California Univ. Berkeley, CA, United States)
Chan, W.-K.
(California, University Berkeley, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Unsteady aerodynamics
Location: Tucson, AZ
Start Date: March 18, 1975
End Date: March 20, 1975
Accession Number
76A10338
Distribution Limits
Public
Copyright
Other

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