References
Bradshaw, P. 1965: The effect of wind tunnel screens on nominally two-dimensional boundary layers. J. Fluid Mech. 22, 679–687
Bradshaw, P. 1972: Two more wind tunnels driven by aerofoil-type centrifugal blowers. Imp. Coll. Aero Rep. 72–10
Furuya, Y.; Nakamura, I.; Osaka, H. 1979: Three-dimensional structure of a nominally planar turbulent boundary layer. ASME J. Fluids Eng. 101, 326–330
Mehta R. D.; Bradshaw, P. 1979: Design rules for small low-speed wind tunnels. Aero. J. Vol. 83, 443–449
Mehta, R. D. 1985: “Turbulent boundary layer perturbed by a screen” AIAA J. 23, 1335–1342 [See also 1984: Turbulent flow through screens. AIAA Paper 84-0538]
Mehta R. D.; Hoffmann, P. H. 1986: A study of the factors affecting boundary layer two-dimensionality in wind tunnels. Dept. of Aeronautics and Astronautics, Stanford University, JIAA Report TR-66
Morgan, P. G. 1960: The stability of flow through porous screens. J. Roy. Aero. Soc. 64, 359–362
Patel, V. C. 1965: Calibration of the Preston tube and limitations on its use in pressure gradients. J. Fluid Mech. 23, 185–208
Perkins, H. J. 1970: The formation of streamwise vorticity in turbulent flow. J. Fluid Mech. 44, 721–740
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Mehta, R.D., Hoffmann, P.H. Boundary layer two-dimensionality in wind tunnels. Exp. Fluids 5, 358 (1987). https://doi.org/10.1007/BF00277718
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF00277718