Raising gas-dynamic stability margin of axial and centrifugal compressor stages by means of vaned diffuser boundary layer control.

Autor:	Lastivka, Ivan1 iola@nau.edu.ua
Zdroj:	Aviation (1648-7788). 2011, Vol. 15 Issue 3, p76-81. 6p.
Databáze:	Academic Search Ultimate
Externí odkaz:	Zobrazit plný text záznamu