Wind-tunnel investigation of the effects of spoilers on the characteristics of a low-drag airfoil equipped with a 0.25-chord slotted flap / by Ralph W. Holtzclaw.

An investigation was made to determine the effects of circular-arc spoilers on the section characteristics of an NACA 66,216 (a = 0.6) airfoil equipped with a 0.25-chord slotted flap. Spoilers were tested on the upper surface of the airfoil at 0.725 chord, on the lower surface at 0.6666 chord, and o...

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Bibliographic Details
Main Author: Holtzclaw, Ralph W.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
Other title:NACA Wartime Reports. Series A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. A92.
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Norlin Library - Basement - Government Information - US

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Call Number: Y 3.N 21/5:11/A92
Y 3.N 21/5:11/A92 Available Place a Hold