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Tests to determine effects of slipstream rotation on the lateral stability characteristics of a single-engine low-wing aircraft model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1946 |
| File Size | 21249256 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081810 |
| Archival Resource Key | ark:/13960/t20c99027 |
| Language | English |
| Publisher Date | 1946-01-01 |
| Access Restriction | Open |
| Subject Keyword | Stability & Control, Lateral Propeller Slipstream - Effect On Stability Wind Tunnel Tests - Corrections, Boundary Tail Surfaces, Vertical Rolling & Yawing Moments Wind Tunnel Tests - Naca (6'x 4') Lmal Stability & Control, Directional Airplanes, Single-engine 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 |