Wind-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes
1945
12 S.
Ill., graph. Darst.
Originally issued April 1945 as Advance restricted report L5B17
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Engineering Index Backfile | 1941
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