Predicting modes of the unsteady vorticity field near the trailing edge of a blade /

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Bibliographic Details
Author / Creator:Devenport, William J.
Imprint:[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor], [2003]
Description:1 volume.
Series:[NASA contractor report] ; NASA/CR-2003-212099
NASA contractor report ; NASA CR-212099.
Aerodynamic noise.
Trailing edges.
Noise prediction (aircraft)
Turbulent boundary layer.
Computational fluid dynamics.
Turbulent flow.
Turbulence models.
Flow distribution.
Format: E-Resource Microform U.S. Federal Government Document Book
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Other authors / contributors:Spitz, Nicolas.
NASA Glenn Research Center.
Notes:Available via Internet from the NASA Technical Reports Server web site. Address as of 10/27/04:; current access available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online) classification:NAS 1.26:212099