Wind-tunnel investigation of control-surface characteristics. : 15 - Various contour modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014 airfoil / by Paul E. Purser and John M. Riebe.

Aerodynamic section characteristics for several flap deflections and for sealed and unsealed gap at the flap nose are presented for true-contour, straight-contour, and beveled trailing edge flaps. Slope of lift curve, flap effectiveness, and negative slope of hinge-moment curves decreased as the tra...

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Bibliographic Details
Main Author: Weil, Joseph
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Riebe, John M.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L668.
Subjects:

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L668
Y 3.N 21/5:11/L668 Available Place a Hold