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Stability and control characteristics at a mach number of 2.01 of a supersonic vtol airplane model having a broad fuselage and small delta wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1961 |
| Description | Stability and control of supersonic vtol airplane model having broad fuselage and small delta wing |
| File Size | 4377677 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630006264 |
| Archival Resource Key | ark:/13960/t4xh4b95j |
| Language | English |
| Publisher Date | 1961-02-01 |
| Access Restriction | Open |
| Subject Keyword | Stability AND Control Fuselage Delta Wing Vtol Aircraft 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 |