Wind-tunnel investigation of control-surface characteristics 17 Beveled-trailing-edge flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil / by Vernard E. Lockwood

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Bibliographische Detailangaben
1. Verfasser: Lockwood, Vernard E. (VerfasserIn)
Format: UnknownFormat
Sprache:eng
Veröffentlicht: Washington, DC NACA, National Advisory Committee for Aeronautics 1944
Schriftenreihe:Wartime report L-666
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Titel Jahr Band
A 0.25-airfoil-chord flap with tab having a chord twice the flap chord on a NACA 0009 airfoil 1945 23
Medium and large aerodynamic balances of two nose shapes and a plain overhung used with a 0.20-airfoil-chord flap on an NACA 0009 airfoil 1945 22
Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil 1945 21
Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface 1944 20
Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps 1944 16
A linked overhang aerodynamic balance 1944 18
Wind-tunnel investigation of control-surface characteristics 17 Beveled-trailing-edge flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil / by Vernard E. Lockwood 1944 L-666
A double flap with an overhang and an internal aerodynamic balance 1944 19
Various large overhang and internal-type aerodynamic balances for a straight-contour flap on the NACA 0015 airfoil 1943 11
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 1943 L-668
Various flap overhangs used with a 30-percent-chord flap on an NACA 66-009 airfoil 1943 13
NACA 0009 airfoil with a 20-percent-chord double plain flap 1943 14
Various cover-plate alinements on the NACA 0015 airfoil with a 30-percent-chord flap and large sealed internal balance 1943 12
A medium aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil 1942 7
A 30-percent-chord plain flap on the NACA 0015 airfoil 1942 6
Some analytical considerations and experimental test results for an internally balanced flap 1942 9
A large aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil 1942 8
The use of a beveled trailing edge to reduce the hinge moment of a control surface 1942 5
A 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil 1942 10
A large aerodynamic balance of various nose shapes with a 30-percent-chrod flap on an NACA 0009 airfoil 1941 2
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