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Analysis of the convergence history of flow through nozzles with shocksAcceleration techniques such as Wynn's (1986) epsilon algorithm and analysis techiques such as eigensystem analysis are used here to study numerically the convergence properties of an iterative scheme applied to the quasi-one-dimensional Euler and Navier-Stokes equations for flow through nozzles with shocks. The convergence and stability properties are studied by analyzing the dependence of convergence of the code on the discretization technique, boundary conditions, time-step, number of grid points, and the physics of the problem.
Document ID
19880061628
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cheer, A. Y.
(California Univ. Davis, CA, United States)
Saleem, M.
(California Univ. Davis, CA, United States)
Hafez, M.
(California, University Davis, United States)
Pulliam, T. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 88-3795
Meeting Information
Meeting: AIAA, ASME, SIAM, and APS, National Fluid Dynamics Congress
Location: Cincinnati, OH
Country: United States
Start Date: July 25, 1988
End Date: July 28, 1988
Accession Number
88A48855
Funding Number(s)
CONTRACT_GRANT: NCA2-172
Distribution Limits
Public
Copyright
Other

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