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William L. Wells

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Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration

by William L. Wells First published in 1990 — 1 edition

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Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FD₄

by William L. Wells First published in 1988 — 1 edition

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Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FDb□-s□b4b□-s□s

by William L. Wells First published in 1988 — 1 edition

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Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air

by William L. Wells First published in 1990 — 1 edition

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OLID: OL4654853A

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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