Dolmatov D. Modeling the operational processes in tangential quite-running aircraft turbine with separating blades

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0407U003016

Thesis Registration Form

0407U003016.pdf

Applicant for

Specialization

  • 05.07.05 - Двигуни та енергоустановки літальних апаратів

08-06-2007

Specialized Academic Board

Д64.062.02

Essay

Object of investigation - aircraft tangential turbine with separating blades; the research purpose - the creating new and the improvement of existent models of work processes in flow part that given way to receive dependences of turbine first stage characteristics from work parameters; research methods are: solid flow math modeling methods, theory of similarity, experimental data work methods; results - development and improvement of the gas flow math model, the creating and tests working turbine; introduction - the work processes calculation algorithm and turbine first testament methodic; the area of implementation - on air engine designs enterprises, scientific institutes of gas flow research.

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Files

D.A.Dolmatov_disser.doc

aref.doc

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