Enhanced design of turbo-jet LPT by separation control using phased plasma actuators /

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Bibliographic Details
Author / Creator:Corke, Thomas C.
Imprint:[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor], [2003]
Description:1 volume.
Series:[NASA contractor report] ; NASA/CR-2003-212294
NASA contractor report ; NASA CR-212294.
Subject:Boundary layer separation.
Separated flow.
Computational fluid dynamics.
Turbine blades.
Pressure distribution.
Flow distribution.
Reattached flow.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6552170
Hidden Bibliographic Details
Other authors / contributors:Thomas, Flint O.
NASA Glenn Research Center.
Notes:"April 2003."
Available via Internet from the NASA Technical Reports Server web site. Address as of 10/26/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030056634%5F2003060710.pdf; current access available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:212294