Three-dimensional flow calculation by the method of characteristics.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4333
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1. Low-Density Shock Tube for Chemical Kinetics Studies
2. Electric Arc-Driven Shock Tube
3. Flow in shock tubes with area change at the diaphragm section
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