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Investigation of a thin wing of aspect ratio 4 in the ames 12-foot pressure wind tunnel iv : the effect of a constant-chord leading-edge flap at high subsonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 16534512 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085607 |
| Archival Resource Key | ark:/13960/t4tj2v690 |
| Language | English |
| Publisher Date | 1949-01-20 |
| Access Restriction | Open |
| Subject Keyword | Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |