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Experiments with a wing from which the boundary layer is removed by suction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1931 |
| Description | This report presents the results of the first investigation of the physical principle of preventing the streamline separation by removing the boundary layer. It was aeronautical, in that it dealt with airfoils, but the results are of a very general application. |
| File Size | 975414 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930094782 |
| Archival Resource Key | ark:/13960/t88h1t06v |
| Language | English |
| Publisher Date | 1931-01-01 |
| Access Restriction | Open |
| Subject Keyword | 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 |