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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of reynolds number at supersonic mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 15186800 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930086361 |
| Archival Resource Key | ark:/13960/t7bs34b7d |
| Language | English |
| Publisher Date | 1950-10-09 |
| 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 |