Computational Modeling for Non-Equilibrium Shock Tube Flows

Bensassi, Khalil ; Brandis, Aaron M ; Cruden, Brett A

关键词: EQUILIBRIUM FLOW;    SHOCK TUBES;    SIMULATION;    COMPUTATIONAL FLUID DYNAMICS;    TIME;    MODELS;    NUMERICAL ANALYSIS;    TEST FACILITIES;   

RP-ID  :  ARC-E-DAA-TN70861

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Time accurate simulation of non-equilibrium flows inside shock tube facilities presents several challenges from both physical and mathematical aspects. Furthermore, the large computational cost makes it impractical to support a real-time experimental test campaign. In this work, we explore other methods for modeling the shock tube problem 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 computationally expensive while still accurate enough with regards to the quantities of interest. Excellent agreement is found with the established stagnation-line approach. Comparison with time-accurate simulations shows good agreement close to the peak values and disagreement of the temperatures relaxation and radiance profiles toward equilibrium.