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Stability and control characteristics at a mach number of 1.97 of an airplane configuration having two types of variable-sweep wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.97 |
| File Size | 18987463 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660022441 |
| Archival Resource Key | ark:/13960/t3c00x68r |
| Language | English |
| Publisher Date | 1960-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Stability Supersonic Wind Tunnel Variable Sweep 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 |