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Reduction of lift of a wing due to its drag
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1935 |
| Description | This analysis computes for a predetermined airfoil and given Reynolds Number the course of the "displacement thickness," i.e., the course of the layer by which the streamlines of the potential flow are pushed away from the wing through the frictional layer. The result is, to a certain extent, a new wing contour. |
| File Size | 5019980 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930094636 |
| Archival Resource Key | ark:/13960/t5bc75d9h |
| Language | English |
| Publisher Date | 1935-01-01 |
| 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 |