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Last edited by ImportBot
September 19, 2008 | History
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William J. Devenport

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4 works Add another?

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  • Cover of: Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

    First published in 1994 — 3 editions
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  • Cover of: Predicting modes of the unsteady vorticity field near the trailing edge of a blade

    First published in 2003 — 2 editions
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  • Cover of: The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction: final technical report ...

    First published in 1997 — 1 edition
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  • Cover of: Velocity measurements in a turbulent trailing vortex and their application to BWI noise prediction

    First published in 1991 — 1 edition
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Subjects

Aerodynamic noise, Blade slap noise, Blade-vortex interaction, Helicopters, Noise prediction, Rotary wings, Aeroacoustics, Blade tips, Computational fluid dynamics, Flow distribution, Incompressible flow, Interactional aerodynamics, Noise, Noise prediction (Aircraft), Statistical distributions, Trailing edges, Turbulence models, Turbulent boundary layer, Turbulent flow, Turbulent wakes, Vortex-motion, Vorticity, Wind tunnel tests

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ID Numbers

  • OLID: OL4866009A

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History

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September 19, 2008 Created by ImportBot Imported from Oregon Libraries MARC record