50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2012
DOI: 10.2514/6.2012-228
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DSMC Modeling of NO Formation for Simulation of Radiation in Hypersonic Flows

Abstract: The current work has implemented in DSMC discrete vibrational levels of N2 and the transitions between them as well as the dissociation of nitrogen molecules and formation of NO molecules. The vibration-translation transition models assessed include LarsonBorgnakke, Schwartz-Slawsky-Herzfeld (SSH), and Forced Harmonic Oscillator (FHO) models. Total Collision Energy (TCE) and QCT models for the NO formation reaction are considered. The effect of the models on the flowfield is explored and comparisons are made. … Show more

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Cited by 10 publications
(1 citation statement)
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“…[1][2][3] For Mach numbers in the range of 13 -20 (moderate Mach numbers), there is sufficient molecular nitrogen dissociation such that the fidelity of the dissociation and vibrational-translational (V-T), vibrational-vibrational (V-V) models significantly impacts the shocklayer features. For lower Mach numbers, 4 there is insufficient dissociation for the dissociation models to play an important role whereas for high Mach numbers (greater than 20, i.e. Stardust reentry flow 5 ), complete dissociation occurs.…”
Section: Introductionmentioning
confidence: 97%
“…[1][2][3] For Mach numbers in the range of 13 -20 (moderate Mach numbers), there is sufficient molecular nitrogen dissociation such that the fidelity of the dissociation and vibrational-translational (V-T), vibrational-vibrational (V-V) models significantly impacts the shocklayer features. For lower Mach numbers, 4 there is insufficient dissociation for the dissociation models to play an important role whereas for high Mach numbers (greater than 20, i.e. Stardust reentry flow 5 ), complete dissociation occurs.…”
Section: Introductionmentioning
confidence: 97%