Wind-tunnel investigation of 20-percent-chord plain and frise ailerons on NACA 23012 airfoil. (Advance Restricted Report Dec 1941)
Wind-tunnel investigation of 20-percent-chord plain and frise ailerons on NACA 23012 airfoil
Nat Advisory Committee Aeronautics -- Wartime Report
1941
14 pages
18 supp plates
Report
English
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Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
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