Performance of Two Types of High Speed, High EfficiencyAxisymmetric Intakes; Journal of Applied and Computational Mechanics; Vol. 7, iss. 1
| Parent link: | Journal of Applied and Computational Mechanics Vol. 7, iss. 1.— 2021.— [P. 93-101] |
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| Awdur Corfforaethol: | |
| Awduron Eraill: | , , , , |
| Crynodeb: | Title screen Performance of two axisymmetric air intakes are compared at conditions suitable for Mach number range from 2 to 8.First is the Busemann intake and second is the reversed isentropic nozzle. The isentropic nozzle is built by the method ofcharacteristics. The contour of this nozzle is taken as a compression surface for the incoming flow. Performances of these twointakes are compared by comparison of both viscous and inviscid CFD calculations at Mach 6. Viscous flow calculations showthat the total pressure recovery in compression section is 0.8316 in the Busemann intake and 0.869 in the reversed isentropicnozzle intake. |
| Iaith: | Saesneg |
| Cyhoeddwyd: |
2021
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| Pynciau: | |
| Mynediad Ar-lein: | https://dx.doi.org/10.22055/jacm.2020.35250.2609 |
| Fformat: | Electronig Pennod Llyfr |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=663019 |
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| 200 | 1 | |a Performance of Two Types of High Speed, High EfficiencyAxisymmetric Intakes |f V. M. Galkin, V. M. Fomin, M. Sannu [et al.] | |
| 203 | |a Text |c electronic | ||
| 300 | |a Title screen | ||
| 330 | |a Performance of two axisymmetric air intakes are compared at conditions suitable for Mach number range from 2 to 8.First is the Busemann intake and second is the reversed isentropic nozzle. The isentropic nozzle is built by the method ofcharacteristics. The contour of this nozzle is taken as a compression surface for the incoming flow. Performances of these twointakes are compared by comparison of both viscous and inviscid CFD calculations at Mach 6. Viscous flow calculations showthat the total pressure recovery in compression section is 0.8316 in the Busemann intake and 0.869 in the reversed isentropicnozzle intake. | ||
| 461 | |t Journal of Applied and Computational Mechanics | ||
| 463 | |t Vol. 7, iss. 1 |v [P. 93-101] |d 2021 | ||
| 610 | 1 | |a электронный ресурс | |
| 610 | 1 | |a труды учёных ТПУ | |
| 610 | 1 | |a supersonic | |
| 610 | 1 | |a air intake | |
| 610 | 1 | |a near-isentropic compression | |
| 610 | 1 | |a total pressure recoveryý | |
| 701 | 1 | |a Galkin |b V. M. |c Geologist |c Associate Professor of Tomsk Polytechnic University, Candidate of physical and mathematical sciences |f 1955- |g Vladislav Mikhailovich |3 (RuTPU)RU\TPU\pers\31674 |9 15811 | |
| 701 | 1 | |a Fomin |b V. M. |c физик |c действительный член РАН (2006), директор ИТПМ СО РАН (с 1989 г.), доктор физико-математических наук (1984), профессор (1987) |f 1940- |g Vasily Mikhaylovich |3 (RuTPU)RU\TPU\pers\33496 | |
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| 701 | 1 | |a Vnuchkov |b D. A. |g Dmitry Aleksandrovich | |
| 701 | 1 | |a Zvegintsev |b V. I. |g Valery Ivanovich | |
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