Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot
Description:
From Summary: "An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift coefficient which could be obtained by providing a model wing with both a Fowler trailing-edge extension flap and a Handley Page type leading-edge slot. A conventional Handley page slot proportioned to operate on the plain wing without a flap gave but a slight increase with the flap; so a special form of slot was developed to work more effectively with the flap. With the best combi…
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Date:
May 1933
Creator:
Weick, Fred E. & Platt, Robert C.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department