NASA NTRS · 19940000561
Measurement Of Crossflow Vortex Structure
Abstract
Method developed for measuring wavelengths of crossflow vortices by using surface-mounted, microthin, multielement hot-film sensors. Provides direct and true value of wavelength of crossflow vortices at various spanwise locations without localized flow disturbances. Attainment of laminar airflow on aircraft wings has significant potential for reducing drag and increasing fuel efficiency.
Keep this discovery
Explore connections, maps & timelines
Maddalon, Dal V., Agarwal, Navel K.. 1994-10-01. Measurement Of Crossflow Vortex Structure. https://ntrs.nasa.gov/citations/19940000561
Cite the original work for its findings. Save a collection to share your selection of sources.