Dynamic Turbine Clearance Simulation Considering the Influence of Temperature on Mechanical Load–Induced Displacements

Author:

Zelenskyi Roman1,Yepifanov Sergiy2,Martseniuk Yevgen3,Kravchenko Igor4,Loboda Igor5

Affiliation:

1. Associate Professor, Dept. of Aircraft Engine Design, National Aerospace Univ., Kharkov Aviation Institute, 17, Chkalov St., Kharkov 61070, Ukraine.

2. Professor, Dept. of Aircraft Engine Design, National Aerospace Univ., Kharkov Aviation Institute, 17, Chkalov St., Kharkov 61070, Ukraine.

3. Senior Lecturer, Dept. of Aircraft Engine Design, National Aerospace Univ., Kharkov Aviation Institute, 17, Chkalov St., Kharkov 61070, Ukraine.

4. Designer General, Zaporozhye Machine-Building Design Bureau Progress State Enterprise Named After Academician A. G. Ivchenko, 2, Ivanova St., Zaporozhye 69068, Ukraine.

5. Profesor Investigador, Escuela Superior de Ingeniería Mecánica y Eléctrica, Instituto Politécnico Nacional, Av. Santa Ana, 1000, Mexico City 04430, México (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference15 articles.

1. ANSYS [Computer software]. ANSYS Canonsburg PA.

2. Archipov A. N. et al. (2009). “The whole-engine model for clearance evaluation.” Proc. ASME Turbo Expo 2009 Orlando FL.

3. Kurzke J. (2011). “Transient simulations during preliminary conceptual engine design.” Proc. 20th ISABE Conf. AIAA Goethenburg Sweden.

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1. Advanced Nonlinear Modeling of Gas Turbine Dynamics;Aerospace Engineering;2019-11-20

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