NASA NTRS · 19810015489
Development of a nonlinear vortex method
Abstract
Progress is reported in the development of reliable nonlinear vortex methods for predicting the steady and unsteady aerodynamic loads of highly sweptback wings at large angles of attack. Abstracts of the papers, talks, and theses produced through this research are included. The modified nonlinear discrete vortex method and the nonlinear hybrid vortex method are highlighted.
Keep this discovery
Explore connections, maps & timelines
Kandil, O. A.. 1981-05-01. Development of a nonlinear vortex method. https://ntrs.nasa.gov/citations/19810015489
Cite the original work for its findings. Save a collection to share your selection of sources.