V -, n ■ 1 1 1 l 1 i i : I i i ' ' t-LU 1^0, .'23; !/ MM! I I - 1 ! I 1 1 -f- "fcTTT 120 lo : 1 .. 1 # I ' 1 _J I . U 100, ! f H> ■ . ! i I I go! 11 … Fig. 3. Polsxe of wings Nos, 358 and 390. E is tiro product of the ohord in mm by the spoed m.p.s. t^ie the 'jing^chord. whioh was 600 mm in the tests between vertioal walls and 200 mm in tne tests oy the usual method.
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