The effect of wind-tunnel screens on nominally two-dimensional boundary layers
- 1 May 1965
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 22 (04), 679-687
- https://doi.org/10.1017/s0022112065001064
Abstract
Spanwise variations of surface shear stress, amounting to 10% or more, may be produced in nominally two-dimensional boundary layers by a spatial instability of the flow through the wind-tunnel damping screens: boundary layers are shown theoretically to be very sensitive to variations of free-stream direction. Screens with open-area ratios more than about 0·57 do not produce appreciable spanwise variations in the boundary layer, and it is recommended that tunnels for boundary-layer measurements should be fitted with such screens. The critical open-area ratio does not seem to depend noticeably on Reynolds number in the usual range encountered in wind tunnels, but the figure of 0·57 should not be taken as general until measurements have been made in representative selection of wind tunnels in other laboratories.Keywords
This publication has 4 references indexed in Scilit:
- Wind-Tunnel Screens: Flow Instability and its Effect on Aerofoil Boundary LayersJournal of the Royal Aeronautical Society, 1964
- The Preston tube as a means of measuring skin frictionJournal of Fluid Mechanics, 1962
- The Stability of Flow Through Porous ScreensJournal of the Royal Aeronautical Society, 1960
- On the Resistance of ScreensAeronautical Quarterly, 1953