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A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at mach numbers from 0.5 to 1.9 (Document No: 19660010454)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft |
| File Size | 4140370 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660010454 |
| Archival Resource Key | ark:/13960/t2992zg39 |
| Language | English |
| Publisher Date | 1957-02-27 |
| Access Restriction | Open |
| Subject Keyword | Fighter Aircraft Stability AND Control Swept Wing Longitudinal Control Lateral Stability 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 |