Инд. авторы:	Kovenya V.M., Slyunyaev A.Y.
Заглавие:	Modeling of supersonic flows near flying vehicle elements
Библ. ссылка:	Kovenya V.M., Slyunyaev A.Y. Modeling of supersonic flows near flying vehicle elements // Journal of Applied Mechanics and Technical Physics. - 2009. - Vol.50. - Iss. 2. - P.251-260. - ISSN 0021-8944. - EISSN 1573-8620.
Внешние системы:	DOI: 10.1007/s10808-009-0034-x; РИНЦ: 13613097; SCOPUS: 2-s2.0-63649163034; WoS: 000264322000011;
Реферат:	eng: Supersonic flows near flying vehicle elements are calculated in the approximation of the full Navier-Stokes equations for a viscous compressible heat-conducting gas with different values of free-stream. Mach and Reynolds numbers and angles of attack. The main laws of the flow near the lifting surface. and in the inlet are obtained.
Издано:	2009
Физ. характеристика:	с.251-260