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The static and dynamic-rotary stability derivatives of a model of the x-15 research airplane at mach numbers from 1.55 to 3.50
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1959 |
| Description | Static and dynamic rotary stability derivatives for X-15 aircraft at supersonic speeds |
| File Size | 2270325 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650003120 |
| Archival Resource Key | ark:/13960/t0sr3m73p |
| Language | English |
| Publisher Date | 1959-01-01 |
| Access Restriction | Open |
| Subject Keyword | X-15 Aircraft Stability Derivative Rotary Stability Aircraft 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 |