NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A modified dodge algorithm for the parabolized Navier-Stokes equations and compressible duct flowsA revised version of a split-velocity method for numerical calculation of compressible duct flow was developed. The revision incorporates balancing of mass flow rates on each marching step in order to maintain front-to-back continuity during the calculation. The (checkerboard) zebra algorithm is applied to solution of the three-dimensional continuity equation in conservative form. A second-order A-stable linear multistep method is employed in effecting a marching solution of the parabolized momentum equations. A checkerboard successive overrelaxation iteration is used to solve the resulting implicit nonlinear systems of finite-difference equations which govern stepwise transition.
Document ID
19810016798
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cooke, C. H.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-164435
Report Number: NASA-CR-164435
Accession Number
81N25334
Funding Number(s)
CONTRACT_GRANT: NSG-1517
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available