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Preconditioning for the Navier-Stokes equations with finite-rate chemistryThe preconditioning procedure for generalized finite-rate chemistry and the proper preconditioning for the one-dimensional Navier-Stokes equations are presented. Eigenvalue stiffness is resolved and convergence-rate acceleration is demonstrated over the entire Mach-number range from the incompressible to the hypersonic. Specific benefits are realized at low and transonic flow speeds. The extended preconditioning matrix accounts for thermal and chemical non-equilibrium and its implementation is explained for both explicit and implicit time marching. The effect of higher-order spatial accuracy and various flux splittings is investigated. Numerical analysis reveals the possible theoretical improvements from using proconditioning at all Mach numbers. Numerical results confirm the expectations from the numerical analysis. Representative test cases include flows with previously troublesome embedded high-condition-number regions.
Document ID
19930039279
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Godfrey, Andrew G.
(NASA Langley Research Center Hampton, VA, United States)
Walters, Robert W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Van Leer, Bram
(Michigan Univ. Ann Arbor, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-0535
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A23276
Funding Number(s)
CONTRACT_GRANT: F49620-92-J-0158
CONTRACT_GRANT: NAG1-776
Distribution Limits
Public
Copyright
Other

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