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

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:

MARC

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260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1944] 
300 |a 14 pages, 45 unnumbered pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L350. 
500 |a NACA Wartime Report L-350. 
500 |a Originally issued as NACA as Advance Confidential Report L4B28 (February 1944) 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a 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 66-009 airfoil. 
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