Flow Nonuniformities Behind Accelerating and Decelerating Shock Waves in Shock Tubes
Author:
Affiliation:
1. University of Oxford, Oxford, England OX1 2 JD, United Kingdom
Funder
Air Force Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060375
Reference28 articles.
1. Diagnostic modelling of an expansion tube operating condition
2. Computational challenges for simulations related to the NASA electric arc shock tube (EAST) experiments
3. Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties
4. Numerical Simulation of Shock Tubes Using Shock Tracking in an Overset Formulation
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