CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /

Bibliographic Details

Main Author:	Vinci, Samuel J. (Author)
Corporate Authors:	Cleveland State University, Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2012.
Series:	NASA contractor report ; NASA CR-2012-217417.
Subjects:	Computational fluid dynamics. Pressure ratio. Boundary layers. Finite volume method. Low speed wind tunnels.
Online Access:	https://purl.fdlp.gov/GPO/gpo33342