Performance of Two Types of High Speed, High EfficiencyAxisymmetric Intakes; Journal of Applied and Computational Mechanics; Vol. 7, iss. 1

Performance of Two Types of High Speed, High EfficiencyAxisymmetric Intakes; Journal of Applied and Computational Mechanics; Vol. 7, iss. 1

Bibliographische Detailangaben
Parent link:Journal of Applied and Computational Mechanics
Vol. 7, iss. 1.— 2021.— [P. 93-101]
Körperschaft: Национальный исследовательский Томский политехнический университет Инженерная школа природных ресурсов Отделение нефтегазового дела
Weitere Verfasser: Galkin V. M. Vladislav Mikhailovich, Fomin V. M. Vasily Mikhaylovich, Sannu M. Molder, Vnuchkov D. A. Dmitry Aleksandrovich, Zvegintsev V. I. Valery Ivanovich
Zusammenfassung: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.
Sprache:Englisch
Veröffentlicht: 2021
Schlagworte:
электронный ресурс
труды учёных ТПУ
supersonic
air intake
near-isentropic compression
total pressure recoveryý
Online-Zugang:https://dx.doi.org/10.22055/jacm.2020.35250.2609
Format: Elektronisch Buchkapitel
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=663019

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