On the theory of the turbulent boundary layer / by J. Rotta.
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1952]
|
| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1344. |
| Subjects: |
| Abstract: | As a rule, a division of the turbulent boundary layer is admissible: a division into a part near the wall, where the flow is governed only by the wall effects, and into an outer part, where the wall roughness and the viscosity of the flow medium affects only the wall shearing stress occurring as boundary condition but does not exert any other influence on the flow. Both parts may be investigated to a large extent independently. Under certain presuppositions there result for the outer part "similar" solutions. The theoretical considerations give a cue how to set up, by appropriate experiments and their evaluation, generally valid connections which are required for the approximate calculation of the turbulent boundary layer according to the momentum and energy theorem. |
|---|---|
| Item Description: | NACA TM Number 1344. Translated from Mitteilungen aus dem Max-Planck-Institut fur Stromungsforschung Gottingen. Number 1, 1950, by the National Advisory Commitee for Aeronautics. |
| Physical Description: | 50 pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |