Inside Out Library · Explore
Collection of wind-tunnel data on commonly used wing sections (1930)
NASA Technical Reports Server (NTRS) · leaf 17
OS LB … Absolute profile drag coefficient, Q,g Fiavsx 47.—Langley Memorial Aeronautical Laboratory tests. Airfoil she 5X30 Inches; aspect ratio, 0. Alrtofl, Olarfc T, average Reynolds Number, 3,810,000; G-387, average Reynolds Number, 3,470,000; M-8, average Reynolds Number, 3,609,000; M-15, average…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Collection of wind-tunnel data on commonly used wing sections
More like this
