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Aerodynamics / Chemical engineering / Boundary layers / Compressors / Axial compressor / Flow separation / Stall / Vortex shedding / Turbine / Fluid mechanics / Fluid dynamics / Aerospace engineering


AIAA[removed]DYNAMIC SEPARATION CONTROL IN A LOW-SPEED ASYMMETRIC DIFFUSER WITH VARYING DOWNSTREAM BOUNDARY CONDITION Samantha H. Feakins, Douglas G. MacMartin, and Richard M. Murray California Institute of Technology
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Document Date: 2003-07-14 18:04:00

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File Size: 244,86 KB

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City

New York / /

Company

Able Corporation / Honeywell / Hemisphere Publishing Corp. / Integrated Inlet/Compression Systems / McCormick / Suzuki / /

Currency

pence / /

Facility

Institute of Aeronautics / Richard M. Murray California Institute of Technology Pasadena / California Institute of Technology / American Institute of Aeronautics / University of Cambridge / /

IndustryTerm

steel plating / steel plate / perforated steel plate / axial flow compression systems / long fiberglass duct / vortex imaging / flow devices / /

NaturalFeature

Near-Isentropic Inlet / /

Organization

California Institute of Technology / G. MacMartin / and Richard M. Murray California Institute of Technology Pasadena / Department of Engineering / University of Cambridge / American Institute of Aeronautics / Institute of Aeronautics and Astronautics / /

Person

Richard M. Murray / Jeremy Pitts / Tom Hynes / Sean Humbert / Samantha H. Feakins / Vikram Mittal / Al Ratner / /

Position

Professor / speaker / /

ProvinceOrState

New York / /

Technology

laser / flow control / Fluid Dynamics / Simulation / /

SocialTag