A Study on Aircraft Structure and Jet Engine

Details A Study on Aircraft Structure and Jet Engine A Study on Aircraft Structure and Jet Engine

Dec 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985jass....2..153p&link_type=abstract

Journal of Astronomy and Space Science, vol. 2, no. 2, p. 153-174.

Astronomy and Astrophysics

Astronomy

Scientific paper

The one of critical factor in gas turbine engine performance is high turbine inlet gas temperature. Therefore, the turbine rotor has so many problems which must be considered such as the turbine blade cooling, thermal stress of turbine disk due to severe temperature gradient, turbine rotor tip clearance, under the high operation temperature. The purpose of this study is to provide the temperature distribution and heat flux in turbine disk which is required to considered premensioned problem by the Finite Difference Method and the Finite Element Methods on the steady state condition.

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