Predicting modes of the unsteady vorticity field near the trailing edge of a blade
By: William J. Devenport and Nicolas Spitz.
Contributors: Spitz, Nicolas.; NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA/CR-2003-212099.; NASA contractor report -- NASA/CR-212099.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information; National Technical Information Service [distributor
Published: 2003
Place of publication: [Cleveland, Ohio]; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Vorticity.; Aerodynamic noise.; Trailing edges.; Noise prediction (Aircraft); Turbulent boundary layer.; Computational fluid dynamics.; Turbulent flow.; Turbulence models.; Flow distribution.
Notes: Shipping list no.: 2003-0490-M.

Also available via Internet from the NASA Technical Reports Server web site. Address as of 10/27/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030022774%5F2003026889.pdf; current access available via PURL.

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