The main elements of a methodology are described that make it possible by mathematical modelling of the condition of a flexible rotor in the design stage to evaluate the effect of the main manufacturing and assembly parameters, and to prescribe their main limits in order to provide prescribed vibrational activity.
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Translated from Izmeritel’naya Tekhnika, No. 7, pp. 39–43, July, 2009.
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Yakubovskii, K.Y. Basis of engineering specifications for a gas-turbine engine rotor. Meas Tech 52, 745–750 (2009). https://doi.org/10.1007/s11018-009-9337-9
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DOI: https://doi.org/10.1007/s11018-009-9337-9