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General solution of Prandtl's boundary-layer equationA method is described by means of which the laminar friction layer at a wall with arbitrary pressure distribution may be calculated from Prandtl's boundary-layer equations.
Document ID
19930093947
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mangler, W
Date Acquired
August 16, 2013
Publication Date
June 1, 1950
Report/Patent Number
NACA-TM-1278
Report Number: NACA-TM-1278
Accession Number
93R23273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER, LAMINAR - WALLS
EQUATIONS - HEAT TRANSMISSION
BOUNDARY LAYER - AIRFOILS
SKIN FRICTION
EQUATIONS - BOUNDARY LAYER - PRANDTL
PRESSURE DISTRIBUTION - WALLS

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