Kukhtin Y. Numerical modelling of unsteady gasdynamic loadings on aero-engine turbine blades

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0407U004084

Thesis Registration Form

0407U004084.pdf

Applicant for

Specialization

  • 05.07.05 - Двигуни та енергоустановки літальних апаратів

28-09-2007

Specialized Academic Board

Д 64.062.02

National Aerospace University "Kharkiv Aviation Institute"

Essay

Rotor blades of aeroengine turbines. Research of the unsteady gasdynamic loadings on rotor bladings of the aeroengine turbine. Of research methods is a methods of computed fluid dynamic. A mathematical model is improved of stationary motion of gas in the shovel crowns. Presented are the results of calculation analysis of unsteady interaction between the rotor blade row and the turbine nozzle vanes row with different spaces. Sphere of use is aviation propulsion engineering; power industry.

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Files

Dissertation--Diss.doc

aref.doc

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