NASA NTRS ยท 19710006352
A numerical solution of the unsteady airfoil with application to the vortex interaction problem
Abstract
Numerical analysis of aerodynamic forces on thin airfoil operating in unsteady potential flow
Keep this discovery
Explore connections, maps & timelines
Rudhman, W. E.. 1970-12-01. A numerical solution of the unsteady airfoil with application to the vortex interaction problem. https://ntrs.nasa.gov/citations/19710006352
Cite the original work for its findings. Save a collection to share your selection of sources.