Accession Number : ADB069068
Title : An Assessment of an Ensemble-Averaged Navier-Stokes Calculation Procedure for Cascade Flow Fields.
Descriptive Note : Final rept. 26 Aug 81-26 Aug 82,
Corporate Author : SCIENTIFIC RESEARCH ASSOCIATES INC GLASTONBURY CT
Personal Author(s) : Shamroth,S. J. ; McDonald,H.
Report Date : AUG 1982
Pagination or Media Count : 58
Abstract : A compressible, time-dependent solution of the Navier-Stokes equations is obtained for both compressor and turbine cascade configurations in subsonic and transonic flows. The analysis uses the Briley-McDonald consistently split linearized block implicit (LBI) procedure to solve the governing equations. Comparisons with measured data are presented which demonstrate the code's ability to predict both subsonic and transonic cascade flow fields.
Descriptors : *Cascades(Fluid dynamics), *Gas turbines, *Compressors, *Mathematical models, *Navier Stokes equations, Subsonic flow, Transonic flow, Flow fields, Mathematical prediction
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE