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Investigation of power gas turbine drives on the basis of mathematical models

  • Aircraft and Rocket Engine Design and Development
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Abstract

A method for investigation of power gas turbine drives on the basis of mathematical models that makes it possible to enhance an information content and precision of existing techniques of power audit is proposed.

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References

  1. Osipov, B.M., Titov, A.V., and Khammatov, A.R., Tool Environment for Gas Turbine Plant Investigation, Vestnik KGTU im. A.N. Tupoleva, 2009, no. 1, pp. 22–24.

  2. Osipov, B.M., Titov, A.V., Tunakov, A.P. et al., Avtomatizirovannoe proektirovanie dvigatelei (Computer-Aided Engine Design), Kazan: Izd. Kazan. Gos, Tekh. Univ., 2005.

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Original Russian Text © B.M. Osipov, A.V. Titov, A.R. Khammatov, 2010, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2010, No. 1, pp. 45–47.

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Osipov, B.M., Titov, A.V. & Khammatov, A.R. Investigation of power gas turbine drives on the basis of mathematical models. Russ. Aeronaut. 53, 69–72 (2010). https://doi.org/10.3103/S1068799810010113

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  • DOI: https://doi.org/10.3103/S1068799810010113

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