Analysing a Numerical Calculation Adequacy of the Recovery Factor for Various Problem Statement Options
<p>The paper studies a recovery temperature distribution in a turbulent boundary layer of the compressible gas in a rectangular heat-insulated channel in supersonic flow mode using the numerical methods of gas dynamics. The software package ANSYS Fluent was used for calculation.<br />In...
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| Format: | Article |
| Language: | Russian |
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MGTU im. N.È. Baumana
2016-01-01
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| Series: | Aèrokosmičeskij Naučnyj Žurnal |
| Subjects: | |
| Online Access: | http://aerospace.elpub.ru:80/jour/article/view/9 |
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