A simple numerical method for the calculation of the laminar boundary layer /
by K. Schröder.

Description

Main Author: Schröder, K.
Related Names: United States. National Advisory Committee for Aeronautics.
Language(s): English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Subjects: Laminar boundary layer.
Aerodynamics.
Summary: An iteration difference method for the calculation of the incompressible laminar boundary layer is described. The method uses Prandtl's boundary layer equation and the boundary conditions directly and permits the attainment of an arbitrary accuracy. The method has been tested successfully in the continuation of the Blasius profile on the flat plate, on the circular cylinder investigated by Heimenz and on an elliptical cylinder of fineness ratio 1:4. The method makes possible the testing of previously developed methods, all of which contain important assumptions.
Note: "Translation of "Ein einfaches numerisches verfahren zur berechnung der laminaren grenzschicht." Zentrale �fr wissenschaftliches Berichtswesen der Luftfahrtforschung des Generalluftzeugmeisters (ZWB) Forschungsbericht Nr. 1741, Berlin-Adlershof, February 25, 1943."
"Report date April 1952."
Also available in electronic format.
Physical Description: 47 p. : ill. ; 27 cm.
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