A study of the stability of the incompressible laminar boundary layer on infinite wedges /
The flow over infinite wedges is investigated theoretically to test a conclusion previously reached by the use of Schlicting's approximate method for calculation of the laminar boundary layer; namely, that in a region of falling pressure a thick velocity profile can be more stable than a thin p...
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1953
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2976 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 2976 |
|---|