Showing 1 - 12 results of 12 for search 'Weiberg, James A.', query time: 0.09s Refine Results
  1. 1
    Section characteristics of an NACA 0006 airfoil with area suction near the leading edge /

    Section characteristics of an NACA 0006 airfoil with area suction near the leading edge / by Weiberg, James A.

    Published 1954
    Government Document Book
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  2. 2
    Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model /

    Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model / by Weiberg, James A.

    Published 1944
    Government Document Book
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  3. 3
    Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage /

    Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage / by Weiberg, James A.

    Published 1945
    Government Document Book
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  4. 4
    Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and area-suction flaps /

    Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and area-suction flaps / by Weiberg, James A.

    Published 1958
    Government Document Book
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  5. 5
    Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane /

    Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane / by Dannenberg, Robert E.

    Published 1955
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  6. 6
    Section characteristics of a 10.5-percent-thick airfoil with area suction as affected by chordwise distribution of permeability /

    Section characteristics of a 10.5-percent-thick airfoil with area suction as affected by chordwise distribution of permeability / by Dannenberg, Robert E.

    Published 1952
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  7. 7
    Effect of type of porous surface and suction velocity distribution on the characteristics of a 10.5-percent-thick airfoil with area suction /

    Effect of type of porous surface and suction velocity distribution on the characteristics of a 10.5-percent-thick airfoil with area suction / by Dannenberg, Robert E.

    Published 1953
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  8. 8
    Perforated sheets as a porous material for distributed suction and injection /

    Perforated sheets as a porous material for distributed suction and injection / by Dannenberg, Robert E.

    Published 1956
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    Government Document Book
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  9. 9
    The resistance to air flow of porous materials suitable for boundary-layer -control applications using area suction /

    The resistance to air flow of porous materials suitable for boundary-layer -control applications using area suction / by Dannenberg, Robert E.

    Published 1954
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  10. 10
    A fibrous-glass compact as a permeable material for boundary-layer-control applications using area suction /

    A fibrous-glass compact as a permeable material for boundary-layer-control applications using area suction / by Dannenberg, Robert E.

    Published 1955
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  11. 11
    Perforated sheets as the porous material for a suction-flap application /

    Perforated sheets as the porous material for a suction-flap application / by Dannenberg, Robert E.

    Published 1957
    Other Authors: “…Weiberg, James A.…”
    Government Document Book
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  12. 12
    Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and blowing flaps /

    Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and blowing flaps / by Griffin, Roy N., Jr

    Published 1958
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