Loading...
Please wait, while we are loading the content...
Similar Documents
An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : static longitudinal stability and control characteristics at a mach number of 1.59
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 10064136 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930086216 |
| Archival Resource Key | ark:/13960/t44r27d2q |
| Language | English |
| Publisher Date | 1950-06-29 |
| 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 |