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Two blowing concepts for roll and lateral control of aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roberts, L. Wood, N. J. Lee, C. S. Tavella, D. A. |
| Copyright Year | 1986 |
| Description | Two schemes to modulate aerodynamic forces for roll and lateral control of aircraft have been investigated. The first scheme, called the lateral blowing concept, consists of thin jets of air exiting spanwise, or at small angle with the spanwise direction, from slots at the tips of straight wings. For this scheme, in addition to experimental measurements, a theory was developed showing the analytical relationship between aerodynamic forces and jet and wing parameters. Experimental results confirmed the theoretically derived scaling laws. The second scheme, which was studied experimentally, is called the jet spoiler concept and consists of thin jets exiting normally to the wing surface from slots aligned with the spanwise direction. |
| File Size | 2388491 |
| Page Count | 108 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870014194 |
| Archival Resource Key | ark:/13960/t9k40p926 |
| Language | English |
| Publisher Date | 1986-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Slots Wings Scaling Laws Wing Tips Roll Spanwise Blowing Aerodynamic Forces Lateral Control Lift Augmentation Spoilers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
