NASA NTRS · 20190028644
Computational Modeling for Non-equilibrium Shock Tube Flows
Abstract
Time accurate simulation of non-equilibrium flows inside shock tube facilities presents several challenges from both physical and mathematical aspects. Furthermore, the drastic computational cost makes it non-practical to support real-time experimental test campaign. In this work, we explore other methods for modeling the shock tube prob- lem with the main focus on the post-shock region and the absolute radiation emanating from it. The proposed alternative approach is several orders of magnitude less computa- tionally expansive while still accurate enough with regards to the quantities of interest. Excellent agreement is found with the well-established stagnation-line approach. Comparison with the time-accurate simulation shows good agreement close to the peak values and disagreement of the temperatures relaxation and radiance profiles toward equilibrium, due to shock speed unsteadiness.
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Bensassi, Khalil, Brandis, Aaron M., Cruden, Brett A.. 2019-07-14. Computational Modeling for Non-equilibrium Shock Tube Flows. https://ntrs.nasa.gov/citations/20190028644
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