Influence of flow conditions over the forebody of a hypersonic air inlet on the flow of air in a boundary-layer bleed channel

In the present paper, we report on the results of a study that was performed as part of the program for developing a method for calculating the flow and the mass-flow-rate coefficient in narrow cylindrical bleed channels under conditions of impingement of a thick boundary layer. For setting the boun...

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Veröffentlicht in:	Thermophysics and aeromechanics 2019-09, Vol.26 (5), p.639-650
Hauptverfasser:	Goldfeld, M. A., Korotaeva, T. A., Obodovskaya, E. A., Turchinovich, A. O.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Air intakes Angle of attack Bleeding Boundary conditions Boundary layers Channels Computational fluid dynamics Computer simulation Domains Forebodies Mass flow Physics Physics and Astronomy Static pressure Temperature profiles Thermodynamics Three dimensional flow Three dimensional models Turbulent flow
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