Autor: |
Podsypanina, N. A., Shifrin, É. G., Shulakov, M. A. |
Zdroj: |
Fluid Dynamics; September 1980, Vol. 15 Issue: 5 p792-793, 2p |
Abstrakt: |
An example is given of calculation of the flow in a two-dimensional Laval nozzle whose profile in the subsonic part is concave with respect to the direction of the oncoming flow. Under the hypothesis of a separationless flow of ideal gas on the walls of the nozzle, regions of deceleration of the flow are absent. Then the well-known criteria suggest the existence of a separationless boundary layer, which must ensure that the flow as a whole is separationless. |
Databáze: |
Supplemental Index |
Externí odkaz: |
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