Loading...
Please wait, while we are loading the content...
Similar Documents
Wind tunnel studies of circulation control elliptical airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Franke, M. E. Harvell, J. K. |
| Copyright Year | 1987 |
| Description | Effects of blown jets on the lift and drag of cambered elliptical airfoils are described. Performance changes due to a splitter plate attached to the lower surface of an elliptical airfoil near the trailing edge with and without blowing are indicated. Lift and drag characteristics of airfoils with two blown jets are compared with airfoils with single blowing jets. Airfoil designs that vary the location of a second jet relative to a fixed jet are described. |
| File Size | 757505 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880008214 |
| Archival Resource Key | ark:/13960/t8gf5pv7k |
| Language | English |
| Publisher Date | 1987-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Under Surface Blowing Ellipticity Aerodynamic Drag Jet Flow Split Flaps Trailing Edges Wind Tunnel Tests Aircraft Performance Aerodynamic Coefficients Circulation Control Airfoils Lift Wing Camber Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
