Effect of Thickened and Beveled Trailing Edges. Wartime Report n A-54 (Advance Confidential Report 4A15 Jan 1944) 18 p. (Advance Confidential Report 4A15 Jan 1944)
Wind tunnel investigation of ailerons on low drag airfoil
Nat Advisory Committee Aeronautics -- Wartime Report
1944
17 pages
46 supp plates, 32 supp plates
Report
Englisch
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Wind-tunnel investigation of drooped ailerons on 16-percent-thick low-drag airfoil
Engineering Index Backfile | 1947
|Wind-tunnel investigation of ailerons on low-drag airfoil. III -- Effect of tabs
Engineering Index Backfile | 1944
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