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LSENS, the NASA Lewis kinetics and sensitivity analysis code
Author(s) -
Krishnan Radhakrishnan
Publication year - 1999
Publication title -
28th joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1999-2394
Subject(s) - sensitivity (control systems) , ordinary differential equation , solver , inviscid flow , shock (circulatory) , chemical kinetics , mathematics , differential equation , computer science , shock tube , thermodynamics , mechanics , statistical physics , physics , mathematical optimization , kinetics , classical mechanics , mathematical analysis , shock wave , engineering , electronic engineering , medicine
A general chemical kinetics and sensitivity analysis code for complex, homogeneous, gas-phase reactions is described. The main features of the code, LSENS (the NASA Lewis kinetics and sensitivity analysis code), are its flexibility, efficiency and convenience in treating many different chemical reaction models. The models include: static system; steady, one-dimensional, inviscid flow; incident-shock initiated reaction in a shock tube; and a perfectly stirred reactor. In addition, equilibrium computations can be performed for several assigned states. An implicit numerical integration method (LSODE, the Livermore Solver for Ordinary Differential Equations), which works efficiently for the extremes of very fast and very slow reactions, is used to solve the "stiff" ordinary differential equation systems that arise in chemical kinetics. For static reactions, the code uses the decoupled direct method to calculate sensitivity coefficients of the dependent variables and their temporal derivatives with respect to the initial values of dependent variables and/or the rate coefficient parameters. Solution methods for the equilibrium and post-shock conditions and for perfectly stirred reactor problems are either adapted from or based on the procedures built into the NASA code CEA (Chemical Equilibrium and Applications).

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