Loading...
Please wait, while we are loading the content...
Similar Documents
High performance forward swept wing aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1988 |
| Description | A high performance aircraft capable of subsonic, transonic and supersonic speeds employs a forward swept wing planform and at least one first and second solution ejector located on the inboard section of the wing. A high degree of flow control on the inboard sections of the wing is achieved along with improved maneuverability and control of pitch, roll and yaw. Lift loss is delayed to higher angles of attack than in conventional aircraft. In one embodiment the ejectors may be advantageously positioned spanwise on the wing while the ductwork is kept to a minimum. |
| File Size | 943946 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880019530 |
| Archival Resource Key | ark:/13960/t77t2kt16 |
| Language | English |
| Publisher Date | 1988-08-30 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Aircraft Stability Supersonic Aircraft Ejectors Aircraft Performance Swept Forward Wings Aircraft Design Aircraft Configurations Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
