NASA NTRS · 19810008577
Active controls for flutter suppression and gust alleviation in supersonic aircraft
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Nissim, E.. 1980-11-01. Active controls for flutter suppression and gust alleviation in supersonic aircraft. https://ntrs.nasa.gov/citations/19810008577
Cite the original work for its findings. Save a collection to share your selection of sources.