Accession Number : AD0262623
Title : EXPERIMENTAL INVESTIGATION ON BOUNDARY LAYER SUCTION BY SERIES OF SLITS AND HOLES
Corporate Author : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)
Personal Author(s) : WUEST, W.
Report Date : APR 1960
Pagination or Media Count : 24
Abstract : The development of laminar and turbulent boundary layers with pressure gradient on various permeable test walls (filter paper, slits, holes, perforations) has been studied in the low-turbulence wind-tunnel of the Aerodynamische Versuchsanstalt. The behaviour of wall-stress, dissipation and the different boundary layer parameters is deduced from the measurements. (Author)
Descriptors : *AERODYNAMIC CHARACTERISTICS, *BOUNDARY LAYER, *BOUNDARY LAYER CONTROL, *LAMINAR BOUNDARY LAYER, *SUBSONIC FLOW, *TURBULENT BOUNDARY LAYER, EXPERIMENTAL DATA.
Distribution Statement : APPROVED FOR PUBLIC RELEASE