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  1. 1
    WInd-tunnel tests of ailerons at various speeds. : 2 - Ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil /

    WInd-tunnel tests of ailerons at various speeds. : 2 - Ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil... by Denaci, H. G.

    Published 1943
    Government Document Book
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  2. 2
    WInd-tunnel tests of ailerons at various speeds. : 5 - Pressure distributions over the NACA 66,2-216 and NACA 23012 airfoils with various balances on 0.20-chord ailerons /

    WInd-tunnel tests of ailerons at various speeds. : 5 - Pressure distributions over the NACA 66,2-216 and NACA 23012 airfoils with various balances on 0.20-chord ailerons / by Letko, W.

    Published 1943
    Other Authors: “…Denaci, H. G.…”
    Government Document Book
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  3. 3
    WInd-tunnel tests of ailerons at various speeds. : 1 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA 66,2-216 airfoil /

    WInd-tunnel tests of ailerons at various speeds. : 1 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA 66,2-216 airfo... by Letko, W.

    Published 1943
    Other Authors: “…Denaci, H. G.…”
    Government Document Book
    Save to List
    Saved in:
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