Interpolation Method Needed for Numerical UncertaintyUsing Computational Fluid Dynamics (CFD) to predict a flow field is an approximation to the exact problem and uncertainties exist. There is a method to approximate the errors in CFD via Richardson's Extrapolation. This method is based off of progressive grid refinement. To estimate the errors, the analyst must interpolate between at least three grids. This paper describes a study to find an appropriate interpolation scheme that can be used in Richardson's extrapolation or other uncertainty method to approximate errors.
Document ID
20130014319
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Groves, Curtis E. (University of Central Florida Orlando, FL, United States)
Ilie, Marcel (University of Central Florida Orlando, FL, United States)
Schallhorn, Paul A. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
January 1, 2014
Subject Category
Numerical Analysis
Report/Patent Number
KSC-2013-136Report Number: KSC-2013-136
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics