Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels
| Parent link: | Journal of Applied Mechanics and Technical Physics: Scientific Journal Vol. 51, iss. 2.— 2010.— [P. 218-225] |
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| Corporate Author: | |
| Other Authors: | , , , |
| Summary: | Title screen A method for design of hypersonic nozzles for wind tunnels is developed and implemented on the basis of solving direct problems with various models of the medium and numerical methods of integration of gas-flow equations. Multimodal nozzles for operation in Mach number ranges Mout = 8-14 and Mout = 14-20 satisfying specified requirements are designed. Режим доступа: по договору с организацией-держателем ресурса |
| Published: |
2010
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| Subjects: | |
| Online Access: | http://dx.doi.org/10.1007/s10808-010-0031-0 |
| Format: | Electronic Book Chapter |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636478 |
| Summary: | Title screen A method for design of hypersonic nozzles for wind tunnels is developed and implemented on the basis of solving direct problems with various models of the medium and numerical methods of integration of gas-flow equations. Multimodal nozzles for operation in Mach number ranges Mout = 8-14 and Mout = 14-20 satisfying specified requirements are designed. Режим доступа: по договору с организацией-держателем ресурса |
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| DOI: | 10.1007/s10808-010-0031-0 |