
Accession Number : ADA310237
Title : SolutionAdaptive Calculation of Unsteady Blade Row Interactions in Transonic Turbomachinery.
Descriptive Note : Final rept. Apr 93Mar 96,
Corporate Author : WRIGHT LAB WRIGHTPATTERSON AFB OH
Personal Author(s) : Richardson, Scott M.
PDF Url : ADA310237
Report Date : MAR 1996
Pagination or Media Count : 232
Abstract : This report describes the development of an implicit, viscous method for the solution of the quasithreedimensional flow equations for rotorstator interaction in transonic turbomachinery. The flow algorithm is described, followed by the implicit timemarching scheme, and the oneequation turbulence model. The algorithm is implemented on an unstructured grid arrangement of locally structured microblocks called 'patches.' Solutiondependent adaptation is used to refine the grid in regions containing flow features which require enhanced resolution. An overlapped sliding grid interface is used to transfer flow equation information between the respective blade grids. The resulting computational algorithm has been used to perform a number of validation exercises and has been demonstrated on a modern transonic turbine stage. Where possible, these results are compared with experimental data and show the ability of the method to accurately capture the unsteady flow physics in a robust and computationally efficient manner.
Descriptors : *COMPUTATIONAL FLUID DYNAMICS, *UNSTEADY FLOW, MATHEMATICAL MODELS, ALGORITHMS, STRESS ANALYSIS, GRIDS, BOUNDARY LAYER, TURBULENCE, TURBULENT FLOW, EDDIES(FLUID MECHANICS), VORTEX SHEDDING, FLOW FIELDS, INTERPOLATION, MACH NUMBER, DRAG, LIFT, NAVIER STOKES EQUATIONS, INVISCID FLOW, VISCOUS FLOW, VISCOSITY, PRESSURE DISTRIBUTION, REYNOLDS NUMBER, SKIN FRICTION, RUNGE KUTTA METHOD, TRANSONIC FLOW, TURBOMACHINERY, COMPRESSOR ROTORS, THREE DIMENSIONAL FLOW, CASCADES(FLUID DYNAMICS), ROTOR BLADES(TURBOMACHINERY), TURBINE STATORS, SMOOTHING(MATHEMATICS).
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE