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The work presents the results of application of a specific method (Group Method of Data Handling) to turbomachines (axial-flow compressors, axial-flow fan and axial-flow gas turbine). The developed statistical models may be especially useful for aviation turbomacnine designers. Results of casing treatment and tandem cascades use in axial-flow compressor are accompanied by detailed experimental test results.

Produktbeschreibung
The work presents the results of application of a specific method (Group Method of Data Handling) to turbomachines (axial-flow compressors, axial-flow fan and axial-flow gas turbine). The developed statistical models may be especially useful for aviation turbomacnine designers. Results of casing treatment and tandem cascades use in axial-flow compressor are accompanied by detailed experimental test results.
Autorenporträt
Main specialization-gas turbine aviation engines. A scientific researcher and lecturer in the National Aerospace University ¿Kharkov Aviation Institute¿ (Ukraine). For seven years a lecturer in the National Polytechnic Institute of Mexico. An invited professor in academic institutions of the USA. Spain and China. Member of the ASME.