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Dynamic stability investigation of two right circular cylinders in axial free flight at mach numbers from 0.4 to 1.7 fineness-ratio-2.56 cylinder and fineness-ratio-4.0 cylinder with flared afterbody
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Dynamic longitudinal stability of right circular cylinders in axial free flight |
| File Size | 1865766 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660024023 |
| Archival Resource Key | ark:/13960/t20c9pf33 |
| Language | English |
| Publisher Date | 1957-02-28 |
| Access Restriction | Open |
| Subject Keyword | Circular Cylinder Free Flight Dynamic Stability Longitudinal 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 |