A numerical simulator for three-dimensional flows through vibrating blade rows [microform] / H. Andrew Chuang and Joseph M. Verdon.

"The three-dimensional, multi-stage, unsteady, turbomachinery analysis, TURBO, has been extended to predict the aeroelastic and aeroacoustic response behaviors of a single blade row operating within a cylindrical annular duct. In particular, a blade vibration capability has been incorporated so...

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Bibliographic Details

Online Access:	Click here to view full text online
Main Author:	Chuang, H. Andrew
Corporate Author:	Lewis Research Center
Other Authors:	Verdon, Joseph M.
Other title:	Numerical simulator for three dimensional flows through vibrating blade rows.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], [1998]
Series:	NASA contractor report ; NASA CR-208511.
Subjects:	Aeroelasticity. Aeroacoustics. Annular ducts. Rotors. Subsonic flow. Three dimensional flow. Transonic flow. Turbomachinery.