Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer

A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ÷ 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given

Генеалогическое древо адмирала Степана Осиповича Макарова: история создания

Мацкевич, В. В. Генеалогическое древо адмирала Степана Осиповича Макарова: история создания = Family tree of the admiral Stepan Osypovych Makarov: history of creation / В. В. Мацкевич, Т. С. Митковская // Shipbuilding & Marine Infrastructure. – 2020. – № 1 (13). – С. 100–104

An experimental study of flow over flat and axisymmetric bodies

The technique and results of an experimental study of the flow structure and critical parameters of the flow over flat and axisymmetric bodies in a range of the Mach numbers (M = 2 ÷ 5) are presented

Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer

A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ÷ 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given