Wind-tunnel investigation of control-surface characteristics. : 18 - A linked overhang aerodynamic balance /

Wind-tunnel investigation of control-surface characteristics. : 18 - A linked overhang aerodynamic balance / by Richard I. Sears and Robert B. Liddell.

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Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a flap balanced by a large overhang linked to deflect more slowly than the flap. Three lengths of blunt-nose overhang were tested linked to a 0.30-airfoil-chord straight-contour flap on an NACA...

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Bibliographic Details
Main Author: Sears, Richard I.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Liddell, Robert B.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L350.
Subjects:
Airplanes > Control surfaces.
Flaps (Airplanes)
Aerofoils.
Wind tunnel testing.
Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L350
Y 3.N 21/5:11/L350 Available Place a Hold

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