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Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 6762504 |
| Page Count | 131 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083028 |
| Archival Resource Key | ark:/13960/t7cs05873 |
| Language | English |
| Publisher Date | 1951-05-01 |
| Access Restriction | Open |
| Subject Keyword | Airplanes - Models - Mass Distribution Spinning - Recovery Spinning Characteristics - Effect OF Wing-tail Combinations Wind Tunnel Tests - Naca - Free-spinning (20 Feet) Spinning Tests - Airplanes, Light 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 |