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Development of a laminar boundary layer behind a suction point
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| Description | A theoretical investigation is made of the development of a laminar boundary layer behind a suction slot that is assumed to cut off part of the boundary layer without exerting any sink effect. The development, which is approximate, is based on the heat conduction equation. The heat conduction equation enters the analysis through a linearization of the Prandtl-Mises form of the boundary-layer equation. |
| File Size | 619180 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093894 |
| Archival Resource Key | ark:/13960/t2n62w939 |
| Language | English |
| Publisher Date | 1952-03-01 |
| Access Restriction | Open |
| Subject Keyword | Equations - Boundary Layer Flow, Laminar Boundary Layer - Stability Boundary Layer Control - Suction - Slots Boundary Layer, Laminar Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |