Use of Refined Finite Element Models for Solving the Contact Thermoalasticity Problem of Gas Turbine Rotors

Author:

Kairov AlekseyORCID, ,Morgun SergeyORCID,

Publisher

National Academy of Sciences of Ukraine (Co. LTD Ukrinformnauka)

Reference7 articles.

1. 1. Pykhalov, A. A. (2007). Staticheskiy i dinamicheskiy analiz sbornykh rotorov turbomashin [Static and dynamic analysis of rotor assembly turbomachines]. Irkutsk: Izd-vo Irkut. tekhn. un-ta, 194 p. (in Russian).

2. 2. Tsvik, L. B. (1980). Printsip poocherednosti v zadachakh o sopryazhenii i kontakte tverdykh deformiruyemykh tel [The principle of succession in problems on the conjugation and contact of solid deformable bodies]. Soviet Applied Mechanics, vol. 16, iss.1, pp. 9−13. https://doi.org/10.1007/BF00884606

3. 3. Gail, P. (1999). Isoparametric finite elements for analysis of shell segments and non-axisymmetric shells. Journal of Sound and Vibration, vol. 65, no. 2, pp. 259−273. https://doi.org/10.1016/0022-460X(79)90519-4

4. 4. Sosunov, V. A. & Chepkin, V. M. (2003). Teoriya, raschet i proyektirovaniye aviatsionnykh dvigateley i energeticheskikh ustanovok [Theory, calculation and design of aircraft engines and power plants]. Moscow: Mosk. energ. in-t, 677 p. (in Russian).

5. 5. Samarskiy A. A. & Vabitsevich P. N. (2009). Vychislitelnaya teploperedacha [Computational heat transfer]. Moscow: Editorial, 784 p. (in Russian).

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