A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers
Wartime report ; L-532
1941
11 S., [11] Bl.
graph. Darst.
Originally issued May 1941 as Memorandum report
Report
Englisch
Boundary Layer and Near-Wake Measurements of NACA 0012 Airfoil at Low Reynolds Numbers
British Library Conference Proceedings | 2009
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