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Wind tunnel investigation of effect of yaw on lateral-stability characteristics iv : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| File Size | 1053418 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092566 |
| Archival Resource Key | ark:/13960/t4gn1dc6z |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Monoplanes, Mid-wing Vs High- & Low-wing Wings, Tapered - Characteristics Effect OF Wing Flaps Rolling & Yawing Moments - Airfoils - Naca 23012 Interferences - Wings & Fuselages Wing Flaps, Split - Partial-span (20% Chord) Wings - Stability, Lateral Fuselages, Circular-wedge-shaped Rear Tail Surfaces, Vertical Stability, Directional 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 |