Tereschenko Y. Models and methods of calculating of the working process of the three pass turbojet engine

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0413U003398

Thesis Registration Form

0413U003398.pdf

Applicant for

Specialization

  • 05.05.03 - Двигуни та енергетичні установки

28-05-2013

Specialized Academic Board

Д 26.062.05

Essay

Common theoretical conditions of working process in principally new type of gas turbine engine had formulated in the dissertation for the first time and math model of the three pass turbojet engine with backside arrangement of turbofan additional unit was built. The includes the math model of turbofan additional unit, that serves for the creation its parameters optimization method. On the basic of numerical solutions, some recommendations on selection and ground working process parameters of three pass turbojet engine are obtained. There is shown the possibility of using this type of engine during creation gas turbine engine on the base of existed gas generator.

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Files

aref.doc

dis.doc

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