NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis and design of numerical schemes for gas dynamics. 2: Artificial diffusion and discrete shock structureThe effect of artificial diffusion on discrete shock structures is examined for a family of schemes which includes scalar diffusion, convective upwind and split pressure (CUSP) schemes, and upwind schemes with characteristics splitting. The analysis leads to conditions on the diffusive flux such that stationary discrete shocks can contain a single interior point. The simplest formulation which meets these conditions is a CUSP scheme in which the coefficients of the pressure differences is fully determined by the coefficient of convective diffusion. It is also shown how both the characteristic and CUSP schemes can be modified to preserve constant stagnation enthalpy in steady flow, leading to four variants, the E and H-characteristic schemes, and the E and H-CUSP schemes. Numerical results are presented which confirm the properties of these schemes.
Document ID
19950005461
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jameson, Antony
(Princeton Univ. NJ., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
RIACS-TR-94-16
NASA-CR-196476
NAS 1.26:196476
Report Number: RIACS-TR-94-16
Report Number: NASA-CR-196476
Report Number: NAS 1.26:196476
Accession Number
95N11874
Funding Number(s)
CONTRACT_GRANT: NAS2-13721
CONTRACT_GRANT: N00014-92-J-1796
CONTRACT_GRANT: AF-AFOSR-0391-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available