NASA NTRS · 19860017730
Viscous vortical flow calculations over delta wings
Abstract
Two approaches to calculate turbulent vortical flows over delta wing configurations are illustrated. The first is for a simple delta wing at low speeds using the boundary layer approximation to treat the effects of the secondary separation. The second is for the supersonic case of a generic fighter using the NASA Ames parabolized Navier/Stokes method. Test/theory comparisons are given in both cases.
Keep this discovery
Explore connections, maps & timelines
Blom, G., Wai, J. C., Yoshihara, H.. 1986-07-01. Viscous vortical flow calculations over delta wings. https://ntrs.nasa.gov/citations/19860017730
Cite the original work for its findings. Save a collection to share your selection of sources.