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Multi-Component Diffusion with Application To Computational AerothermodynamicsThe accuracy and complexity of solving multicomponent gaseous diffusion using the detailed multicomponent equations, the Stefan-Maxwell equations, and two commonly used approximate equations have been examined in a two part study. Part I examined the equations in a basic study with specified inputs in which the results are applicable for many applications. Part II addressed the application of the equations in the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA) computational code for high-speed entries in Earth's atmosphere. The results showed that the presented iterative scheme for solving the Stefan-Maxwell equations is an accurate and effective method as compared with solutions of the detailed equations. In general, good accuracy with the approximate equations cannot be guaranteed for a species or all species in a multi-component mixture. 'Corrected' forms of the approximate equations that ensured the diffusion mass fluxes sum to zero, as required, were more accurate than the uncorrected forms. Good accuracy, as compared with the Stefan- Maxwell results, were obtained with the 'corrected' approximate equations in defining the heating rates for the three Earth entries considered in Part II.
Document ID
20040090466
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sutton, Kenneth
(NASA Langley Research Center Hampton, VA, United States)
Gnoffo, Peter A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 98-2575
Report Number: AIAA Paper 98-2575
Meeting Information
Meeting: 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
Location: Albuquerque, NM
Country: United States
Start Date: June 15, 1998
End Date: June 18, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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