Spatial transformations for reacting gas shock tube experiments
Shock tube flows can be used to investigate nonequilibrium thermochemistry and radiative processes found in hypersonic flows. The flow in a shock tube contains many flow nonuniformities, in particular boundary-layer effects. For the purpose of studying the properties of the test slug, the flow behin...
Main Authors: | , , |
---|---|
Format: | Journal article |
Language: | English |
Published: |
American Institute of Aeronautics and Astronautics
2023
|