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Effect of winglets on a first-generation jet transport wing. 2: pressure and spanwise load distributions for a semispan model at high subsonic speeds. [in the langley 8 ft transonic tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Flechner, S. G. Montoya, L. C. Jacobs, P. F. |
| Copyright Year | 1977 |
| Description | Pressure and spanwise load distributions on a first-generation jet transport semispan model at high subsonic speeds are presented for the basic wing and for configurations with an upper winglet only, upper and lower winglets, and a simple wing-tip extension. Selected data are discussed to show the general trends and effects of the various configurations. |
| File Size | 9010628 |
| Page Count | 212 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780012122 |
| Archival Resource Key | ark:/13960/t2p60cb4k |
| Language | English |
| Publisher Date | 1977-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Drag Subsonic Speed Winglets Transport Aircraft Transonic Wind Tunnels Jet Aircraft Semispan Models Pressure Distribution Wind Tunnel Models Wing Profiles Wing Loading Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
