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Wind-tunnel investigation of the static and dynamic-rotary stability derivatives of a flat-top wing-body model at mach numbers of 2.5, 3.0 and 3.5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Endicott, K. C. Lampkin, B. A. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1960 |
| Abstract | Wind tunnel investigation of static and dynamic- rotary stability derivatives of flat-top wing body |
| File Size | 6603031 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19630008112 |
| Archival Resource Key | ark:/13960/t8x92w87z |
| Language | English |
| Publisher Date | 1960-04-01 |
| Access Restriction | Open |
| Subject Keyword | Body-wing Configurations Rotary Stability Static Stability Wind Tunnel Stability Test Wing Body Sideslip Stability Derivatives Supersonic Speed Wind Tunnel Stability Tests Wind Tunnels Wings Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |