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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : subsonic mach and reynolds number effects on the characteristics of the wing and on the effectiveness of an elevon
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 27851997 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085437 |
| Archival Resource Key | ark:/13960/t9g491n7q |
| Language | English |
| Publisher Date | 1948-10-11 |
| 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 |