Showing 1 - 9 results of 9 for search 'Chu, Julio', query time: 0.03s Refine Results
  1. 1
    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges

    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges by Chu, Julio

    Published 1996
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  2. 2
    High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

    High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions by Chu, Julio

    Published 1990
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  3. 3
    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° /

    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° / by Mulcay, William, Chu, Julio

    Published 1980
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  4. 4
    Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /

    Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges / by Chu, Julio, Luckring, James M.

    Published 1996
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    Online Access
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  5. 5
    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°

    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° by Mulcay, William

    Published 1980
    Other Authors: “…Chu, Julio…”
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  6. 6
    High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

    High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

    Published 1990
    Other Authors: “…Chu, Julio…”
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  7. 7
    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊.

    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊. by Hultberg, Randy S.

    Published 1980
    Other Authors: “…Chu, Julio…”
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  8. 8
    Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers /

    Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers / by Tracy, M. B.

    Published 1992
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  9. 9
    Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds

    Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds by Plentovich, Elizabeth B.

    Published 1991
    Other Authors: “…Chu, Julio…”
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