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Mach number distribution over the axis of supersonic underexpanded jets |
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| Authors: | Yu P Finat'ev L A Shcherbakov N M Gorskaya |
| Affiliation: | (1) Institute of Chemical Physics, Academy of Sciences of the USSR, Moscow |
| Abstract: | The limiting flow parameters are determined directly behind the central shock for Mach numbers M ? 1 in front of the shock. A formula for the Mach number distribution over the jet axis is derived. |
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