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Lift and drag effects of wing-tip rake
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1923 |
| Description | This report deals with a description and report of tests carried out at the Washington Navy Yard on models of the RAF-6, albatross and Slone airfoils to determine the effectiveness of the conventional wing-trailing edge being always longer than the leading edge. The results are compared with the values computed by standard formulae in use at the time the tests were conducted. |
| File Size | 447392 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930091205 |
| Archival Resource Key | ark:/13960/t6p01bx08 |
| Language | English |
| Publisher Date | 1923-01-01 |
| 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 |