Showing 1 - 10 results of 19 for search 'Letko, William', query time: 0.08s Refine Results
  1. 1
    Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /
    by Letko, William, Letko, William
    Published 1963

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  2. 2
    Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /
    by Letko, William, Letko, William
    Published 1960

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  3. 3
    Theoretical investigation at subsonic speeds of the flow ahead of a slender inclinded parabolic-arc body of revolution and correlation with experimental data obtained at low speeds /
    by Letko, William
    Published 1954

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  4. 4
    Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations /
    by Letko, William
    Published 1958

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  5. 5
    Wind-tunnel investigation of split trailing-edge lift and trim flaps on a tapered wing with 23 degrees sweepback /
    by Letko, William
    Published 1947

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  6. 6
    Effect of vertical-tail area and length on the yawing stability characteristics of a model having a 45 degree sweptback wing /
    by Letko, William
    Published 1951

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  7. 7
    Investigation of the fuselage interference on a pitot-static tube extending forward from the nose of the fuselage /
    by Letko, William
    Published 1947

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  8. 8
    A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslip /
    by Letko, William
    Published 1953

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  9. 9
    Experimental investigation at low speed of the effects of wing position on the static stability of models having fuselages of various cross section and unswept and 45 degree sweptback surfaces /
    by Letko, William
    Published 1956

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  10. 10
    Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61 /
    by Letko, William
    Published 1948

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