Гапонов, С. А.; Ермолаев, Ю. Г.; Косинов, А. Д.; Семенов, Н. В.; Смородский, Б. В.
(Новосибирский государственный университет, 2008)
Theoretical and an experimental research results of the disturbances development in a swept wing boundary layer are presented at Mach number М = 2. In experiments development of natural and small amplitude controllable ...