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Effect of an alternate winglet on the pressure and spanwise load distributions of a first generation jet transport wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Flechner, S. G. Montoya, L. C. Jacobs, P. F. |
| Copyright Year | 1978 |
| Description | Pressure and spanwise load distributions on a first-generation jet transport semispan model at subsonic speeds are presented. The wind tunnel data were measured for the wing with and without an alternate winglet. The results show that the winglet affected outboard wing pressure distributions and increased the spanwise loads near the tip. |
| File Size | 3291713 |
| Page Count | 96 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790005841 |
| Archival Resource Key | ark:/13960/t8gf5m874 |
| Language | English |
| Publisher Date | 1978-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Subsonic Speed Winglets Transport Aircraft Jet Aircraft Wind Tunnel Tests Semispan Models Pressure Distribution Load Distribution Forces Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
