Modelling of axial - turbine characteristics of an aircraft engine

• Autorzy: Antas, S. , Kujda, J.
• Konferencja: International Conference SYMKOM '99. Compressor & Turbine Stage Flow Path Theory, Experiment & User Verification (1999 ; Łódź, Polska)
• Języki publikacji: EN

Abstrakty

EN

This paper presents the model and black diagram of a programme enabling to determine characteristics of a reaction axial-turbine of an aircraft engine. The method used for description of flow phenomena with applying the criterion of similarity of thrmogasdynamics processes brings to an iterative solution of algebraic equations system. The T62003 programme made by WSK „PZL-Rzeszów” S.A. enables to make full theoretical analysis of influence of rims geometrical size and aerodynamic stream values on the turbine characteristics pattern. The Mukhtarov's model elaborated by CIAM was used to determine aerodynamic losses.

Słowa kluczowe

EN

aircraft engine; axial turbine; modelling

• Czasopismo: Zeszyty Naukowe. Cieplne Maszyny Przepływowe - Turbomachinery / Politechnika Łódzka
• Rocznik: 1999
• Tom: nr 115
• Strony: 21--30
• Opis fizyczny: Bibliogr. 11 poz.

Twórcy

autor

Antas, S.

• Transport Equipment Enterprise WSK „PZL-Rzeszów” S.A.

autor

Kujda, J.

• Transport Equipment Enterprise WSK „PZL-Rzeszów” S.A.