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Fast and optimal solution to the Rankine-Hugoniot problemA new, definitive, reliable and fast iterative method is described for determining the geometrical properties of a shock (i.e., theta sub Bn, yields N, V sub s and M sub A), the conservation constants and the self-consistent asymptotic magnetofluid variables, that uses the three dimensional magnetic field and plasma observations. The method is well conditioned and reliable at all theta sub Bn angles regardless of the shock strength or geometry. Explicit proof of uniqueness of the shock geometry solution by either analytical or graphical methods is given. The method is applied to synthetic and real shocks, including a bow shock event and the results are then compared with those determined by preaveraging methods and other iterative schemes. A complete analysis of the confidence region and error bounds of the solution is also presented.
Document ID
19850022411
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Vinas, A. F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Scudder, J. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Numerical Analysis
Report/Patent Number
NASA-TM-86214
REPT-85B0392
NAS 1.15:86214
Report Number: NASA-TM-86214
Report Number: REPT-85B0392
Report Number: NAS 1.15:86214
Accession Number
85N30724
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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