Loading...
Please wait, while we are loading the content...
Similar Documents
Active controls for flutter suppression and gust alleviation in supersonic aircraft. [yf-17 flutter model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nissim, E. |
| Copyright Year | 1980 |
| Description | Results of work done on active controls on the modified YF-17 flutter model are summarized. The basic derivation of a suitable control law is discussed. It is shown that discrepencies found between analysis and wind tunnel tests originate from the lack of proper implementation of the desired control law. Program capabilities are described. |
| File Size | 11521896 |
| Page Count | 270 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810008577 |
| Archival Resource Key | ark:/13960/t6g20sx03 |
| Language | English |
| Publisher Date | 1980-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control F-17 Aircraft Vibration Damping Supersonic Cruise Aircraft Research Gust Alleviators Transfer Functions Wind Tunnel Tests Eigenvalues Mathematical Models Flutter Analysis Equations of Motion Active Control Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |