Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
By: Thomas C. Corke and Flint O. Thomas.
Contributors: Thomas, Flint O.; NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA/CR-2003-212294.; NASA contractor report -- NASA/CR-212294.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Administration; National Technical Information Service [distributor
Published: 2003
Place of publication: [Cleveland, Ohio]; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Boundary layer separation.; Separated flow.; Computational fluid dynamics.; Turbine blades.; Pressure distribution.; Flow distribution.; Actuators.; Reattached flow.
Notes: Shipping list no.: 2002-0490-M.

"April 2003."

Also 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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003?] 1 microfiche.