3D CFD Research of Labyrinth Seal Cavities of Aircraft Turbine Engine

Čížek, Michal

doi:10.1109/ntad.2019.8875611

2019 New Trends in Aviation Development (NTAD) 2019

DOI: 10.1109/ntad.2019.8875611

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3D CFD Research of Labyrinth Seal Cavities of Aircraft Turbine Engine

Michal Čížek¹

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Labyrinth Seal of Aircraft Turbine Engine Air Flow Calculation at High Viscosity

Čížek¹,

Vampola²

2019

Acta Mechanica Slov.

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This paper describes a CFD calculation of aircraft turbine engine labyrinth seal. The geometry of labyrinth seal shows that the air flow is very viscous. Based on the CFD calculation it was prepared some analysis of Reynolds numbers, Mach numbers and total temperature with different rotational speeds. Based on this analysis it is possible to improve the standard design steps of labyrinth seals of aircraft turbine engines. It should be helpful for thermodynamic and aircraft engineers.

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Labyrinth Seal of Aircraft Turbine Engine Air Flow Calculation at High Viscosity

Čížek¹,

Vampola²

2019

Acta Mechanica Slov.

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3D CFD Research of Labyrinth Seal Cavities of Aircraft Turbine Engine

Cited by 1 publication

References 6 publications

Labyrinth Seal of Aircraft Turbine Engine Air Flow Calculation at High Viscosity

Labyrinth Seal of Aircraft Turbine Engine Air Flow Calculation at High Viscosity

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