Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations. Progress report, 1 December 1985-31 May 1986
Technical Report
·
OSTI ID:6921429
The two-dimensional Navier-Stokes and species continuity equations are used to investigate supersonic chemically reacting flow problems which are related to scramjet-engine configurations. A global two-step finite-rate chemistry model is employed to represent the hydrogen-air combustion in the flow. An algebraic turbulent model is adopted for turbulent flow calculations. The explicit unsplit MacCormack finite-difference algorithm is used to develop a computer program suitable for a vector processing computer. The computer program developed is then used to integrate the system of the governing equations in time until convergence is attained. The chemistry source terms in the species continuity equations are evaluated implicitly to alleviate stiffness associated with fast chemical reactions. The problems solved by the elliptic code are re-investigated by using a set of two-dimensional parabolized Navier-Stokes and species equations. A linearized fully-coupled fully-implicit finite difference algorithm is used to develop a second computer code which solves the governing equations by marching in spce rather than time, resulting in a considerable saving in computer resources. Results obtained by using the parabolized formulation are compared with the results obtained by using the fully-elliptic equations. The comparisons indicate fairly good agreement of the results of the two formulations.
- Research Organization:
- Old Dominion Univ., Norfolk, VA (USA)
- OSTI ID:
- 6921429
- Report Number(s):
- N-87-10187; NASA-CR-179800; NAS-1.26:179800
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
37 INORGANIC, ORGANIC, PHYSICAL, AND ANALYTICAL CHEMISTRY
400800* -- Combustion
Pyrolysis
& High-Temperature Chemistry
ALGORITHMS
CHEMICAL REACTION KINETICS
CHEMICAL REACTIONS
COMBUSTION KINETICS
COMPUTER CODES
DATA
ELEMENTS
FLUID FLOW
HYDROGEN
INFORMATION
KINETICS
MATHEMATICAL LOGIC
MATHEMATICS
NONMETALS
NUMERICAL ANALYSIS
NUMERICAL DATA
REACTION KINETICS
THEORETICAL DATA
THERMODYNAMICS
TURBULENT FLOW
400800* -- Combustion
Pyrolysis
& High-Temperature Chemistry
ALGORITHMS
CHEMICAL REACTION KINETICS
CHEMICAL REACTIONS
COMBUSTION KINETICS
COMPUTER CODES
DATA
ELEMENTS
FLUID FLOW
HYDROGEN
INFORMATION
KINETICS
MATHEMATICAL LOGIC
MATHEMATICS
NONMETALS
NUMERICAL ANALYSIS
NUMERICAL DATA
REACTION KINETICS
THEORETICAL DATA
THERMODYNAMICS
TURBULENT FLOW