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Theoretical investigation of the dynamic lateral stability characteristics of douglas design no. 39c, an early version of the x-3 research airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| Description | Contains results of calculations made to determine the neutral oscillatory stability boundaries, period and time to damp of the oscillatory mode, and motions following disturbances. The calculations were made for Mach numbers of 0.75 and 2.3 at an attitude of 35,000 feet and for the landing condition at sea level. |
| File Size | 1190750 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085567 |
| Archival Resource Key | ark:/13960/t2x39464f |
| Language | English |
| Publisher Date | 1949-01-18 |
| Access Restriction | Open |
| Subject Keyword | Stability - Lateral AND Directional - Dynamic Stability, Lateral - Static Damping Derivatives - Stability Flying Qualities Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |