Diseño preliminar de un rotor de onda para motores con microturbina

Authors

  • Gina P. Pérez B. Universidad de San Buenaventura
  • Arnold Escobar G. Instituto Militar Aeronáutico

DOI:

https://doi.org/10.18667/cienciaypoderaereo.53

Keywords:

Termodinamica, cámara de combustion, rotor de onda

Abstract

This article shows the benefits of using a wave rotor on small turbo jet engine (J.lT), designed and built at San Buenaventura University [6}. The investigation is focused in a design method that obtains the correct geometry using thermodynamic calculus. CFD (Computational Fluid Dynamics) is used to eyaluate the viability in the engine. The equations for the wave rotor preliminary calculus are found through this paper. The input data for the wave rotor design is  supported in basic thermodynamic calculus of the engine without the wave rotor.

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Author Biographies

  • Gina P. Pérez B., Universidad de San Buenaventura

    Grupo de investigación motor combustión GIMOC categoría B colciencias, Universidad de San Buenaventura- Bogotá

  • Arnold Escobar G., Instituto Militar Aeronáutico

    Grupo de investigación en tecnología y desarrollo en logística y seguridad aérea, GITELS registrado en Colciencias, Instituto Militar Aeronáutico- Fuerza Aérea Colombiana

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Published

2009-01-01

How to Cite

Diseño preliminar de un rotor de onda para motores con microturbina. (2009). Ciencia Y Poder Aéreo, 4(1), 38-41. https://doi.org/10.18667/cienciaypoderaereo.53