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Time-split finite-volume method for three-dimensional blunt-body flowAn efficient numerical method for calculating plane, axisymmetric, and fully three-dimensional blunt-body flow is presented. It is a second-order-accurate, time-dependent finite-volume procedure that solves the Euler equations in integral conservation-law form. These equations are written with respect to a Cartesian coordinate system in which an embedded mesh adjusts in time to the motion of the bow shock that is automatically captured as part of the weak solution. With such an adjusting mesh, oscillations in flow properties near the shock are shown to be virtually eliminated. The scheme uses a time-splitting concept that accelerates the convergence appreciably. Comparisons are made between computed and experimental results.
Document ID
19740027801
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rizzi, A. W.
Inouye, M.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 73-133
Report Number: AIAA PAPER 73-133
Accession Number
74A10551
Distribution Limits
Public
Copyright
Other

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