Development of mathematical model and computer program for primary design of transonic axial compressor
The mathematical model underlying the program for calculating and designing axial compressors is presented. The process of calculating the pressure loss in the elements of the axial compressor stage flow path is described. The loss coefficient consists of losses on the limiting surfaces, secondary...
Similar Items
-
New version of Universal modeling method for centrifugal compressors calculation development
by: Yu. B. Galerkin, et al.
Published: (2019-06-01) -
CFD INVESTIGATION OF IMPELLER DIFFUSER INTERACTION EFFECTS ON RADIAL COMPRESSOR STAGE
by: Kumlu, Armagan
Published: (2014) -
Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed
by: Jakob P. Haug, et al.
Published: (2018-02-01) -
Aerodynamic Design Optimization of a Micro Radial Compressor of a Turbocharger
by: Omer Faruk Atac, et al.
Published: (2018-07-01) -
Modeling the Design Flow Coefficient of a Centrifugal Compressor Impeller
by: A. A. Drozdov, et al.
Published: (2017-01-01)