NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Investigation of Convection and Pressure Treatment with Splitting TechniquesTreatment of convective and pressure fluxes in the Euler and Navier-Stokes equations using splitting formulas for convective velocity and pressure is investigated. Two schemes - controlled variation scheme (CVS) and advection upstream splitting method (AUSM) - are explored for their accuracy in resolving sharp gradients in flows involving moving or reflecting shock waves as well as a one-dimensional combusting flow with a strong heat release source term. For two-dimensional compressible flow computations, these two schemes are implemented in one of the pressure-based algorithms, whose very basis is the separate treatment of convective and pressure fluxes. For the convective fluxes in the momentum equations as well as the estimation of mass fluxes in the pressure correction equation (which is derived from the momentum and continuity equations) of the present algorithm, both first- and second-order (with minmod limiter) flux estimations are employed. Some issues resulting from the conventional use in pressure-based methods of a staggered grid, for the location of velocity components and pressure, are also addressed. Using the second-order fluxes, both CVS and AUSM type schemes exhibit sharp resolution. Overall, the combination of upwinding and splitting for the convective and pressure fluxes separately exhibits robust performance for a variety of flows and is particularly amenable for adoption in pressure-based methods.
Document ID
19950017979
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Thakur, Siddharth
(Florida Univ. Gainesville, FL., United States)
Shyy, Wei
(NASA Lewis Research Center Cleveland, OH, United States)
Liou, Meng-Sing
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-106868
E-9483
ICOMP-95-3
NAS 1.15:106868
Report Number: NASA-TM-106868
Report Number: E-9483
Report Number: ICOMP-95-3
Report Number: NAS 1.15:106868
Accession Number
95N24399
Funding Number(s)
CONTRACT_GRANT: NCC3-370
PROJECT: RTOP 505-90-5K
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available