Doroshenko K. Gasdynamic flow control in compressors of gas turbine engines

Українська версія

Thesis for the degree of Doctor of Science (DSc)

State registration number

0518U000237

Thesis Registration Form

0518U000237.pdf

Applicant for

Specialization

  • 05.05.03 - Двигуни та енергетичні установки

11-10-2018

Specialized Academic Board

Д 26.062.05

National Aviation University

Essay

The theory of gas turbine engines in the direction of research of the parameters and characteristics of axial-flow compressors of gas turbine engines with gasdynamic flow control was further developed in paper. In thesis a scientific - methodological apparatus was created to solve the scientific - applied problem of providing gas-dynamic stability and efficiency of ax-ial-flow compressors of gas turbine engines by gas-dynamic flow control in the compressor. A technique for determining of the stall line of a compressor with gasdynamic flow control was developed using generalized characteristics of flow locking modes in the last stages of the axial-flow compressor.

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Files

aref.doc

dis.doc

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