Performance of Two Types of High Speed, High EfficiencyAxisymmetric Intakes

Sonraí bibleagrafaíochta
Parent link:Journal of Applied and Computational Mechanics
Vol. 7, iss. 1.— 2021.— [P. 93-101]
Údar corparáideach: Национальный исследовательский Томский политехнический университет Инженерная школа природных ресурсов Отделение нефтегазового дела
Rannpháirtithe: Galkin V. M. Vladislav Mikhailovich, Fomin V. M. Vasily Mikhaylovich, Sannu M. Molder, Vnuchkov D. A. Dmitry Aleksandrovich, Zvegintsev V. I. Valery Ivanovich
Achoimre: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.
Teanga:Béarla
Foilsithe / Cruthaithe: 2021
Ábhair:
Rochtain ar líne:https://dx.doi.org/10.22055/jacm.2020.35250.2609
Formáid: Leictreonach Caibidil leabhair
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=663019

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