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Pressure Distribution Over a Clark Y-H Airfoil Section with a Split Flap

Carl J. Wenzinger

出版	National Advisory Committee for Aeronautics, 1937
URL	http://books.google.com.hk/books?id=rnhDAQAAIAAJ&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

An investigation was made in the N.A.C.A. 7- by 10-foot wind tunnel of the distributions of air pressure over one chord section of the Clark Y-H airfoil with a split flap. The results obtained are given in the form of diagrams showing the chordwise distribution of pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap.