Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons (1929)
NASA Technical Reports Server (NTRS) · leaf 21
N.A.O.A. Technical Note ITo . 51S Fig.9 11 0 -2° 0 '11o -5° 1 a' 0° n a n , 3b 'It0 b 5° 30- o c ;i7° 35 a 10 P … Drag coefficient,Cn Fig.9 Force polars,ailerons setting with two stablo positions,
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