A detailed laminar flow field within the normal shock wave considering variable specific heats, viscosity and Prandtl numbers
The gas flow field within an 1D normal shock wave at variable specific heats, viscosity and Prandtl numbers with temperature is considered. At Pr = 0.75 and constant specific heats and viscosity, the already known analytical solution in a somehow different form is found. At some distance from the wa...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2013-03-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/berbente_c__berbente_s__brebenel_m__full.pdf |