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Effect of winglets on a first-generation jet transport wing. 3: pressure and spanwise load distributions for a semispan model at mach 0.30. [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 a Mach number of 0.30 are given for the basic wing and for configurations with an upper winglet only, upper and lower winglets, and a simple wing-tip extension. To simulate second-segment-climb lift conditions, leading- and/or trailing-edge flaps were added to some configurations. |
| File Size | 3388618 |
| Page Count | 103 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780012120 |
| Archival Resource Key | ark:/13960/t8hf2n15m |
| Language | English |
| Publisher Date | 1977-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Drag Subsonic Wind Tunnels Subsonic Speed Winglets Transport Aircraft Jet Aircraft Semispan Models Pressure Distribution Wind Tunnel Models Wing Profiles Trailing Edge Flaps 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 |
