Showing 1 - 9 results of 9 for search 'Bihrle, William', query time: 0.03s Refine Results
  1. 1
    Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane /

    Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane / by Bihrle, William

    Published 1951
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  2. 2
    Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes /

    Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes / by Bihrle, William

    Published 1950
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  3. 3
    A Handling qualities theory for precise flight path control /

    A Handling qualities theory for precise flight path control / by Bihrle, William

    Published 1966
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  4. 4
    Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30̊ to 90̊ /

    Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30̊ to 90̊ / by Bihrle, William

    Published 1978
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  5. 5
    Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8̊ to 90̊ /

    Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8̊ to 90̊ / by Bihrle, William

    Published 1978
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  6. 6
    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel /

    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel / by Stone, Ralph W., Bihrle, William, Burk, Sanger M.

    Published 1950
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  7. 7
    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8̊ to 90̊ /

    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8̊ to 90̊ /

    Published 1979
    Other Authors: “…Bihrle, William…”
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  8. 8
    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel /

    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel / by Stone, Ralph W., Jr

    Published 1950
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  9. 9
    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8̊to 90̊ /

    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8̊to 90̊ /

    Published 1979
    Other Authors:
    Search for the full-text version of this title in HathiTrust
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