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Fixed wing ccw aerodynamics with and without supplementary thrust deflection
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Harris, M. J. Nichols, J. H. |
| Copyright Year | 1987 |
| Description | The concept of circulation control was successfully demonstrated in flight using an A-6 aircraft. Circulation control can provide an aircraft with STOL performance of heavy lift capability. For ship based Naval aircraft the lower takeoff and landing velocities result in reduced deck gear and wind over the deck requirements. Circulation control airfoils can be mechanically less complex and lightweight compared to multi-element high lift airfoils. |
| File Size | 4268680 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880008223 |
| Archival Resource Key | ark:/13960/t0ps2p89w |
| Language | English |
| Publisher Date | 1987-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Weight Reduction Fixed Wings Trailing Edges A-6 Aircraft Thrust Distribution Aerodynamic Coefficients Short Takeoff Aircraft Circulation Control Airfoils Lift Augmentation Flow Deflection Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
