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Investigation of effect of sideslip on lateral stability characteristics i : circular fuselage with variations in vertical-tail area and tail length with and without horizontal tail surface
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1944 |
| File Size | 17195804 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092565 |
| Archival Resource Key | ark:/13960/t31293f1k |
| Language | English |
| Publisher Date | 1944-01-01 |
| Access Restriction | Open |
| Subject Keyword | Tail Surfaces - Area Stability & Control, Lateral Sideslipping Tail Surfaces, Vertical Cones, Tail Yawing Moments Tail Surfaces, Horizontal Wind Tunnel Tests - Naca - Stabilty Lmal Fuselages, Circular 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 |