Wind-Tunnel Investigation of Rectangular NACA 2212 Airfoil with Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aerodynamic Brakes. (Originally issued as Advance Restricted Report L5B17)
Wind-tunnel investigation of rectangular NACA 2212 airfoil with semispan Ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes
Nat Advisory Committee Aeronautics -- Wartime Report
1945
12 pages
5 Supp Plates
Report
Englisch
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Engineering Index Backfile | 1941
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