NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
New integration techniques for chemical kinetic rate equations. 2: Accuracy comparisonA comparison of the accuracy of several techniques recently developed for solving stiff differential equations is presented. The techniques examined include two general purpose codes EEPISODE and LSODE developed for an arbitrary system of ordinary differential equations, and three specialized codes CHEMEQ, CREKID, and GCKP84 developed specifically to solve chemical kinetic rate equations. The accuracy comparisons are made by applying these solution procedures to two practical combustion kinetics problems. Both problems describe adiabatic, homogeneous, gas phase chemical reactions at constant pressure, and include all three combustion regimes: induction, heat release, and equilibration. The comparisons show that LSODE is the most efficient code - in the sense that it requires the least computational work to attain a specified accuracy level. An important finding is that an iterative solution of the algebraic enthalpy conservation equation for the temperature can be more accurate and efficient than computing the temperature by integrating its time derivative.
Document ID
19850005489
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Radhakrishnan, K.
(Michigan Univ. Ann Arbor, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:86893
E-2366
NASA-TM-86893
Report Number: NAS 1.15:86893
Report Number: E-2366
Report Number: NASA-TM-86893
Meeting Information
Meeting: Intern. Gas Turbine Conf. and Exhibit,
Location: Houston, TX
Country: United States
Start Date: March 17, 1985
End Date: March 21, 1985
Sponsors: ASME
Accession Number
85N13798
Funding Number(s)
PROJECT: RTOP 505-33-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available