ON MAGNETOHYDRODYNAMIC FLOW SPACES (in Russian)
Journal Article
·
· Priklad. Mat. i Mekhan.
OSTI ID:4838592
It is shown that there are two hyperbolic regions of flow for an ideal gas in the presence of a magnetic field parallel to the velocity of the gas stream. In the supersonic hyperbolic region, the flow is comparable to the usual gasdynamic supersonic flow. In the subsonic hyperbolic region, shock waves are emitted from the upper surface of the stream as evidenced by flow maps. Within the limits of linear theory, it is shown that not only are shock waves emitted but also vortical sheets. These are related to the usual aerodynamic equations describing such flow. Extensions are derived covering cases of quasi-hyperbolic regions. (TTT)
- Research Organization:
- Originating Research Org. not identified
- NSA Number:
- NSA-15-030161
- OSTI ID:
- 4838592
- Journal Information:
- Priklad. Mat. i Mekhan., Journal Name: Priklad. Mat. i Mekhan. Vol. Vol: 25
- Country of Publication:
- Country unknown/Code not available
- Language:
- Russian
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