Abstract
In this paper, under consideration is the complex approach to analyzing the operation of a simulator for the hollow blade made from the VT6 titanium alloy. The stress state parameters in the hollow-monolithic part transition zone of the cantilevered simulator at bending under the distributed load are determined.
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Original Russian Text © V.K. Berdin, A.M. Smyslov, N.V. Berdin, V.V. Luk’yanov, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 123-125.
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Berdin, V.K., Smyslov, A.M., Berdin, N.V. et al. Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades. Russ. Aeronaut. 59, 134–137 (2016). https://doi.org/10.3103/S1068799816010219
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DOI: https://doi.org/10.3103/S1068799816010219