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Slotted aircraft wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2006 |
| Description | A swept aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one full-span slot is defined by the wing during at least one transonic condition of the wing. The full-span slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition. |
| File Size | 3764187 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20060050044 |
| Archival Resource Key | ark:/13960/t0jt4n069 |
| Language | English |
| Publisher Date | 2006-05-23 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Slots Airfoils Transonic Flow Swept Wings Leading Edges Trailing Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
