Determination of the profile drag of an airplane wing in flight at high Reynolds numbers (1939)
NASA Technical Reports Server (NTRS) · leaf 6
DETERMINATION OF PROFILE DRAG OF AIRPLANE WING IN FLIGHT AT HIGH REYNOLDS NUMBERS 3 Figure 2.—Original wing. F , Flush rivets, 3/^2 ' inch diameter L , Lap Joint, facing backward R , Brazier -head rivets, 3/3g - inch diameter r .Brazier-head rivets, l/ig-inch diameter b , Brazier-head rivets,… … Percent chord Figube~3.—Detailsof surface irregularities ou original wing. 147268-39 2
NASA Technical Reports Server (NTRS)
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