Designing and developing new aerospace propulsion systems is time-consuming and expensive. Computational simulation is a promising means for alleviating this, due to the flexibility it provides for rapid and relatively inexpensive evaluation of alternative designs, and because it can be used to integrate multidisciplinary analysis earlier in the design process. In this paper a numerical method based on CFD computations for predicting the performances given by turbine engines during transients is presented.

A Computational Method for Gas Turbine Engines / Marsilio, Roberto. - (2005). (Intervento presentato al convegno 43rd AIAA Aerospace Sciences Meeting and Exhibit tenutosi a Reno, Nevada (USA) nel 10-13 January 2005).

A Computational Method for Gas Turbine Engines

MARSILIO, Roberto
2005

Abstract

Designing and developing new aerospace propulsion systems is time-consuming and expensive. Computational simulation is a promising means for alleviating this, due to the flexibility it provides for rapid and relatively inexpensive evaluation of alternative designs, and because it can be used to integrate multidisciplinary analysis earlier in the design process. In this paper a numerical method based on CFD computations for predicting the performances given by turbine engines during transients is presented.
2005
9781563476068
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/1414617
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