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Spanwise transition section for blended wing-body aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1999 |
| Description | A blended wing-body aircraft includes a central body, a wing, and a transition section which interconnects the body and the wing on each side of the aircraft. The two transition sections are identical, and each has a variable chord length and thickness which varies in proportion to the chord length. This enables the transition section to connect the thin wing to the thicker body. Each transition section has a negative sweep angle. |
| File Size | 568503 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080004521 |
| Archival Resource Key | ark:/13960/t3fz2706v |
| Language | English |
| Publisher Date | 1999-06-08 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Sweep Angle Patents Aircraft Design Wings Transition Points Blended-wing-body Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
