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/j2 ' inc^ diameter L , Lop Joint, facing backward R , Brazier -head rivets, 3/32 ~ ,nch diameter r , Brazier-head rivets, IjiQ-inch diameter b , Brazier-head rivets} 3/32-inch diameter, not extending across wing but in survey pi one D , Trailing edge of…
NASA Technical Reports Server (NTRS)
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