Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder (1927)
NASA Technical Reports Server (NTRS) · leaf 15
M.A.C.A. Technical Memorandum No.411 Figs.1, 2 a, Model b, Hot-wire anemometer c, Micrometer screw for adjusting .//ire perpendicular to chord d, Micrometer screw for adjusting wire parallel to chord ' e, Fitot tube f, Electric motor fc5r driving the .cylinder g, Driving cord h, Tungsten lamp i,… … Fig.2 Arrangement of apparatus for pressure-distribution measurements•
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
