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A theory for lateral wing-tip blowing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roberts, L. Tavella, D. |
| Copyright Year | 1985 |
| Description | The concept of lateral blowing consists in utilizing thin jets of air, which are ejected in the spanwise direction from slots at the tips of straight and swept wings, or along the leading edges of delta wings, to generate aerodynamic forces without the assistance of deflecting solid surfaces. For weak intensities of blowing the so-generated forces could be used for roll and lateral control of aircraft. In this work a theory for this concept as applied to straight wings is presented, revealing the analytical relationship between blowing and aerodynamic forces. The approach is based on perturbing the span of an elliptically loaded wing. Scaling laws involving blowing intensity, aspect ratio, and angle of attack are derived and compared with experiments. It is concluded that this concept has potential as a novel roll and lateral control device. |
| File Size | 735494 |
| Page Count | 41 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860019451 |
| Archival Resource Key | ark:/13960/t7wm65c7n |
| Language | English |
| Publisher Date | 1985-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Swept Wings Delta Wings Rectangular Wings Wing Tips Spanwise Blowing Angle of Attack Aerodynamic Forces Aspect Ratio Lateral Control Leading Edges Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
