51st AIAA/SAE/ASEE Joint Propulsion Conference 2015
DOI: 10.2514/6.2015-4226
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Diagnostic Investigation of Flame Spread Mechanism in Dual-thrust Solid Propellant Rocket Motors

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“…where For the high Reynolds number form of the k-ω model, a * = a * ∞ = 1. Ω ij is the average rate of rotation tensor and the blending functions, F 1 and F 2 , are given by [18,22,23]:…”
Section: Effective Diffusivity Modelmentioning
confidence: 99%
“…where For the high Reynolds number form of the k-ω model, a * = a * ∞ = 1. Ω ij is the average rate of rotation tensor and the blending functions, F 1 and F 2 , are given by [18,22,23]:…”
Section: Effective Diffusivity Modelmentioning
confidence: 99%