Martin Riedler

(Former)

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Research output

  1. Published

    A closed concept to associate the hot-forging process controlled microstructure with fatigue life

    Stoschka, M., Stockinger, M., Maderbacher, H. & Riedler, M., 2 Oct 2012, Superalloys 2012 - Proceedings of the 12th International Symposium on Superalloys. p. 625-631 7 p.

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  2. Published

    A High Cycle Fatigue Model for Al-Alloys based on Low Cycle Fatigue Data and Notch Sensitivity

    Riedler, M., Araujo, B., Leitner, H. & Eichlseder, W., 2005, A High Cycle Fatigue Model for Al-Alloys based on Low Cycle Fatigue Data and Notch Sensitivity. DAS Secretariat, p. 178-179

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  3. Published

    Analysis and simulation of heat treatment processes for fatigue and fracture optimization of forged aircraft engine and structural parts

    Riedler, M., Stockinger, M., Stoschka, M., Oberwinkler, B., Tan, W. & Leitner, H., 2009, Aeromat2009. p. 11-12

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  4. Published

    A new lifetime calculation method based on variation of the microstructure due to different manufacturing conditions of Ti-6Al-4V

    Tan, W., Stoschka, M., Riedler, M. & Eichlseder, W., 2010, 18th European Conference on Fracture Fracture of Materials and Structures from Micro to Macro Scale. p. 0-1

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  5. Published

    An integrated approach to relate hot forging process controlled microstructure of IN718 aerospace components to fatigue life

    Stoschka, M., Riedler, M., Stockinger, M., Maderbacher, H. & Eichlseder, W., 2010, 7th International Symposium on SUPERALLOY718 and DERIVATIVES. p. 751-765

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  6. Published

    Applicability of plastic and total hysteresis energy criterions for simulating the TMF lifetime

    Riedler, M., Winter, G., Minichmayr, R. & Eichlseder, W., 2005, Applicability of plastic and total hysteresis energy criterions for simulating the TMF lifetime. p. 35-35

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  7. Published

    Assessment of lifetime calculation of forged IN718 aerospace components based on a mulit-parametric microstructural evaluation

    Stoschka, M., Stockinger, M., Leitner, H., Riedler, M. & Eichlseder, W., 2008, SUPERALLOYS 2008. p. 573-582

    Research output: Chapter in Book/Report/Conference proceeding › Chapter › Research

  8. Published

    Assessment of lifetime calculation of forged IN718 aerospace components based on a multi-parametric microstructural evaluation

    Stoschka, M., Stockinger, M., Leitner, H. & Riedler, M., 2008, Eleventh International Symposium on Superalloys. p. 573-582

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  9. Published

    Bruchmechanische Lebensdauerbewertung von geschmiedeten Bauteilen aus Ti-6Al-4V

    Oberwinkler, B., Leitner, H. & Riedler, M., 2008, DVM Bericht 642, Tagung Werkstoffprüfung 2008. p. 257-262

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  10. Published

    Cast Iron Versus Aluminium Cylinder Head Materials: Their Properies Concerning to Thermo Mechanical Fatigue

    Winter, G., Riedler, M., Minichmayr, R. & Eichlseder, W., 2005, Cast Iron Versus Aluminium Cylinder Head Materials: Their Properies Concerning to Thermo Mechanical Fatigue. p. 196-197

    Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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