Tests carried out on NACA 2414.5 wing section over range of airplane speeds giving max Reynolds Number of 15,000,000; tests also made to locate point of transition from laminar to turbulent boundary layer and to determine velocity distribution along upper surface of wing.
Determination of profile drag of airplane wing in flight at high Reynolds numbers
Nat Advisory Committee Aeronautics -- Report
1939
9 pages
Bibliography
Report
English
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