Investigation in N.A.C.A. 7 by 10-ft wind tunnel to find increase in maximum lift coefficient obtained by providing model wing with both Fowler trailing-edge extension flap and Handley Page type leading-edge slot; with best combined arrangement max lift coefficient based on original area increased from 3.17, for Fowler wing, to 3.62.
Wind-tunnel tests on model wing with fowler flap and specially developed leading-edge clot
Nat Advisory-Committee Aeronautics -- Tech Note
1933
10 pages
7 Supp sheets
Report
Englisch
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