| Abstract: | The pattern of the flow in the vicinity of an annular system of jets exiting into a supersonic stream from orifices on a cylindrical
surface with a turbulent boundary layer is experimentally investigated Four typical flow regimes are recorded The effect of
the jet number and the nozzle-to-outer pressure ratio on the extent of the separation zone and its structure ahead of and
behind the jet system is determined
Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 21–27, January–February,
1999. |
