Basic data consisting of contours of control location for maximum section lift coefficient and for minimum profile drag coefficient for various control deflections also presented.
Wind-tunnel investigation of drooped ailerons on 16-percent-thick low-drag airfoil
Nat Advisory Committee Aeronautics -- Tech Note
1947
25 pages
44 Supp Sheets
Report
Englisch
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Wind tunnel investigation of ailerons on low drag airfoil
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