Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression

Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression

Xehetasun bibliografikoak
Parent link:	Journal of Applied Mechanics and Technical Physics.— , 1965- Vol. 56, iss. 5.— 2015.— [P. 831-837]
Egile nagusia:	Galkin V. M. Vladislav Mikhailovich
Erakunde egilea:	Национальный исследовательский Томский политехнический университет (ТПУ) Институт природных ресурсов (ИПР) Кафедра геологии и разработки нефтяных месторождений (ГРНМ)
Beste egile batzuk:	Vnuchkov D. A., Zvegintsev V. I.
Gaia:	Title screen A method of designing a supersonic axisymmetric tunnel air inlet based on the problem of an inverted flow in an annular nozzle with isentropic expansion is considered. The nozzle contour is constructed by the method of characteristics. Parameters of one inlet for viscous and inviscid gas flows are calculated. Режим доступа: по договору с организацией-держателем ресурса
Hizkuntza:	ingelesa
Argitaratua:	2015
Gaiak:	электронный ресурс труды учёных ТПУ
Sarrera elektronikoa:	http://dx.doi.org/10.1134/S0021894415050090
Formatua:	Baliabide elektronikoa Liburu kapitulua
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=645703

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