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High speed wind-tunnel investigation of the longitudinal stability and control characteristics of a 1/16-scale model of the d-558-2 research airplane at high subsonic mach number and at a mach number of 1.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 14833702 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085883 |
| Archival Resource Key | ark:/13960/t9v16ch1d |
| Language | English |
| Publisher Date | 1949-04-05 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |