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Wind Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics: [Part] 4 - Symmetrically Tapered Wing With a Circular Fuselage Having a Wedge-Shaped Rear and a Vertical Tail
| Content Provider | University of North Texas |
|---|---|
| Author | Recant, I. G. Wallace, Arthur R. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting testing of combinations of an NACA 23012 tapered wing and a circular fuselage with a wedge-shaped rear to determine the effect of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. Results regarding the lateral stability at small and large angles of yaw are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc61016 |
| Language | English |
| Publisher Date | 2019-03-13 |
| Access Restriction | Open |
| Subject Keyword | wing-fuselage interference aircraft stability aerodynamics |
| Content Type | Text |
| Resource Type | Report |