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Timothy R. Moes

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Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers

by Timothy R. Moes First published in 1993 — 4 editions

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In-flight investigation of shuttle tile pressure orifice installations

by Timothy R. Moes First published in 1990 — 4 editions

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Wind-tunnel development of an SR-71 aerospike rocket flight test configuration

by Timothy R. Moes First published in 1996 — 1 edition

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Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

by Timothy R. Moes First published in 1997 — 1 edition

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A preliminary look at techniques used to obtain airdata from flight at high angles of attack

by Timothy R. Moes First published in 1990 — 1 edition

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Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights

by Timothy R. Moes First published in 1991 — 1 edition

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OLID: OL4664496A

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Created September 14, 2008
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September 14, 2008

Created by ImportBot

Imported from Oregon Libraries MARC record