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Julio Chu

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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 Julio Chu First published in 1990 — 4 editions

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Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds

by Julio Chu First published in 1987 — 1 edition

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Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

by Julio Chu First published in 1996 — 1 edition

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Pressure measurements on a thick cambered and twisted 58ʻ́

by Julio Chu First published in 1987 — 1 edition

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OLID: OL4654358A

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Created September 13, 2008
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September 13, 2008

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Imported from Oregon Libraries MARC record