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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 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.
Document ID
20190028644
Acquisition Source
Ames Research Center
Document Type
Conference Paper
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
August 1, 2019
Publication Date
July 14, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARC-E-DAA-TN70486
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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