Have a personal or library account? Click to login
Thermal Fatigue Problems of Turbine Casing Cover
Open Access
|Sep 2010

References

  1. MSC Corporation(2007). MARC-2005 User_s Manual. Los Angeles: MSC Corporation.
  2. MSC Corporation(2005). MARC-2005 User_s Manual, ver. 2005r2. Los Angeles: MSC Corporation
  3. Michailov, P. B.(1961). Sprawocznik po Metaliczeskim Matierialam Turbino- i Motorostroenija, Petersburg.
  4. Ngii, D. M.(2007). Stress and strain analysis of the PZL-10W turbine casing. Master's Thesis, Rzeszów: Rzeszów University of Technology, Faculty of Mechanical Engineering and Aeronautics.
  5. Witek, L.(2006). Failure analysis of turbine disc of an aero engine, Engineering Failure Analysis, 13(1), Elsevier Science.10.1016/j.engfailanal.2004.12.028
  6. Witek, L., Kowalski, T., & Mamrowicz, J.(2007). Numerical stress and fatigue analysis of the first stage of turbine for helicopter engine. In: Proceedings of the International Conference on Aeronautical Fatigue, Napoli.
  7. Witek, L., Poznańska, A., & Wierzbińska, M. Fracture analysis of a compressor blade of a helicopter engine, Engineering Failure Analysis, 16(5), 1616-1622.10.1016/j.engfailanal.2008.10.022
  8. Witek, L.(2009). Experimental crack propagation and failure analysis of the first stage compressor blade subjected to vibration. Engineering Failure Analysis. 16(7), 2163-2170.10.1016/j.engfailanal.2009.02.014
DOI: https://doi.org/10.2478/v10164-010-0018-6 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 205 - 211
Published on: Sep 23, 2010
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2010 Lucjan Witek, Daniel Ngii, Tadeusz Kowalski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2009 (2009): Issue 1 (July 2009)