Research related to understanding and modeling aerodynamic loss production in axial-flow compressors was accomplished. Some progress in clarification of loss prediction was attained. Suggestions for incorporating wake interaction effects in axial-flow compressor design calculations are offered. Some of the inherent complications associated with supersonic blade testing are noted. Further study of specific details of loss generation is proposed.
Aerodynamic Loss Sources in Axial-Flow Compressors
1986
38 pages
Report
No indication
English
Jet & Gas Turbine Engines , Axial flow compressors , Aerodynamics , Losses , Sources , Computations , Fluid mechanics , Models , Production , Flow , Measurement , Turbomachinery , Axial flow , Predictions , Blades , Supersonic characteristics , Test methods , Interactions , Wake , Turbine blades , Aerodynamic losses
Aerodynamic Design of Axial-Flow Compressors
NTRS | 1965
|Aerodynamic design and axial flow compressors
TIBKAT | 1965
|Aerodynamic design and axial flow compressors
SLUB | 1965
|Aerodynamic Design of Axial Flow Compressors and Turbines
Springer Verlag | 1968
|