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.
Measurement Of Crossflow Vortex Structure
NASA Tech Briefs ; 18 , 10
1994-10-01
Miscellaneous
No indication
English
Measurement of Crossflow Vortex Structure
Online Contents | 1994
The Effect of Crossflow on Vortex Rings
AIAA | 2007
|The Nonlinear Instability of the Supersonic Crossflow Vortex
British Library Conference Proceedings | 2014
|Ground vortex formed by impinging jets in crossflow
AIAA | 1993
|