Демин А.

Thesis for the degree of

State registration number

0497U001443

0497U001443.pdf

Date of defense

26-06-1997

Д 02.27.05

Thesis supervisor

Official opponents

Kirchu Fedor Ivanovich

Optimization of gap channel geometrical parameters of transonic axial compressor with tandem blade row

Koorosh Khaghani

Selection technique of rational parameters highly-loaded blade rows of gas-turbine engine axial-flow compressor

Kukhtin Yuriy

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

Dolmatov Dmitriy Anatolievich

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

Petrov Alexey Vladimirovich

Service life designing of aircraft GTE fan blades with taking into account contact interaction in the joints