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Computational Modeling for Non-Equilibrium Shock Tube FlowsTime 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.
Document ID
20190027559
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Bensassi, Khalil
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Brandis, Aaron M.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Cruden, Brett A.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
July 21, 2019
Publication Date
July 14, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARC-E-DAA-TN70861
Meeting Information
Meeting: International Symposium on Shock Waves (ISSW32)
Location: Singapore
Country: China
Start Date: July 14, 2019
End Date: July 19, 2019
Sponsors: National Univ. of Singapore
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
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