Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition
Only a limited number of free-stream flow properties can be measured in hypersonic impulse facilities at the nozzle exit. This poses challenges for experimenters when subsequently analysing experimental data obtained from these facilities. Typically in a reflected shock tunnel, a simple analysis tha...
| Main Authors: | , , |
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| Format: | Journal article |
| Language: | English |
| Published: |
2013
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