Calculating of blade aerodynamic wake behind the compressor grating
DOI:
https://doi.org/10.15587/1729-4061.2011.1442Keywords:
Аerodynamic wake, uneven flow, compressor gratingAbstract
The problem of calculating the basic parameters of the aerodynamic wake behind the trailing edge of blades of compressor grating gas turbine engine is considered in the work
References
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