Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods; Journal of Engineering Physics and Thermophysics; Vol. 82, iss. 6
| Parent link: | Journal of Engineering Physics and Thermophysics: Scientific Journal Vol. 82, iss. 6.— 2009.— [P. 1127-1131] |
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| Yhteisötekijä: | |
| Muut tekijät: | , , , |
| Yhteenveto: | Title screen On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8-14 and 14-20 satisfying given conditions have been designed. Режим доступа: по договору с организацией-держателем ресурса |
| Kieli: | englanti |
| Julkaistu: |
2009
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| Aiheet: | |
| Linkit: | http://dx.doi.org/10.1007/s10891-010-0306-6 |
| Aineistotyyppi: | Elektroninen Kirjan osa |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636476 |