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Last edited by ImportBot
September 13, 2008 | History
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Julio Chu

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4 works Add another?

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  • Cover of: 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

    First published in 1990 4 editions in 1 language
    Not in Library

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  • Cover of: Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

    First published in 1996 1 edition in 1 language
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  • Cover of: Pressure measurements on a thick cambered and twisted 58ʻ́

    First published in 1987 1 edition in 1 language
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  • Cover of: Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds

    First published in 1987 1 edition
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We need a photo of Julio Chu

Subjects
Delta wings, Subsonic speed, Aerodynamics, Airplanes, Delta wing airplanes, Leading edges, Mach number, Pressure distribution, Reynolds number, Slender wings, Transonic wind tunnels, Vortices, Wind tunnel tests, Wings

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ID Numbers

  • OLID: OL4654358A

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History

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September 13, 2008 Created by ImportBot Imported from Oregon Libraries MARC record