Ing.

Petr Augustin

Ph.D.

FME, IAE DAT – Assistant professor

+420 54114 2558, +420 54114 3468
augustin@fme.vutbr.cz

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Ing. Petr Augustin, Ph.D.

Publications

  • 2018

    AUGUSTIN, P. Simulation of Fatigue Crack Propagation in the Wing Main Spar Flange. In 13th Research and Education in Aircraft Design Conference. 2018. p. 66-75. ISBN: 978-80-214-5696-9.
    Detail

    AUGUSTIN, P. Fatigue life analysis of aging aircraft based on previous service usage. In New Trends in Civil Aviation. Leiden, The Netherlands: CRC Press/Balkema, 2018. p. 113-118. ISBN: 978-0-8153-7602-6.
    Detail | WWW

    JETELA, V.; KLEMENT, J.; AUGUSTIN, P. The possibility for improving damage tolerance of integral airframe structure by high strength bonded straps. Manufacturing TECHNOLOGY, 2018, vol. 18, no. 4, p. 572-577. ISSN: 1213-2489.
    Detail | WWW

  • 2017

    JETELA, V.; KLEMENT, J.; AUGUSTIN, P. Possibility for improving damage tolerance of integral structure by high strength bonded straps. In 14th Seminar "Materials and technologies in Special Technics Production 2017". Brno: University of Defence, 2017. p. 29-33. ISBN: 978-80-7231-420-1.
    Detail

  • 2016

    KATRŇÁK, T.; AUGUSTIN, P.; VLČEK, D. Fatigue analyses and optimization of L 410 NG aircraft. Letecký zpravodaj, 2016, vol. 2016, no. 2, p. 39-41. ISSN: 1211-877X.
    Detail | WWW

  • 2015

    J. KLEMENT, P. AUGUSTIN. Damage tolerance of high-speed machined integral panels made from 2024- T351 aluminium alloy. In XIII. Odborný seminář Materiály a technologie ve výrobě speciální techniky. Brno: Univerzita obrany, Brno, 2015. p. 52-59. ISBN: 978-80-7231-999- 2.
    Detail

  • 2010

    KUNZ, J.; KOVÁŘÍK, O.; LAUSCHMANN, H.; SIEGL, J.; AUGUSTIN, P. Fractographic reconstitution of fatigue crack growth in integrally stiffened panels. Procedia Engineering, 2010, vol. 2, no. 1, p. 1711-1720. ISSN: 1877- 7058.
    Detail

    KLEMENT, J.; AUGUSTIN, P.; URÍK, T. Damage tolerance behaviour of fibre metal laminate CARE. Letecký zpravodaj, 2010, vol. 2010, no. 1, p. 56-59. ISSN: 1211- 877X.
    Detail

  • 2009

    JURAČKA, J.; AUGUSTIN, P.; KOULA, V. Zkoušky únavového chování segmentu křídla. Transfer, 2009, vol. 2009, no. 9, p. 33-45. ISSN: 1801- 9315.
    Detail

    LAUSCHMANN, H.; AUGUSTIN, P.; KOVÁŘÍK, O.; ŠIŠKA, F. The Reference Crack Growth Rate: An Unifying Concept for Fatigue under Variable Amplitude Loading. In Proceedings of the Second International Conference on Material and Component Performance under Variable Amplitude Loading. Darmstadt: Deutscher Verband für Materialforschung und -prüfung, 2009. p. 271-280. ISBN: 978-3-00-027049-9.
    Detail

    AUGUSTIN, P. Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading. In Fatigue of Aircraft Structures. Monographic Series. Warsaw: Institute of Aviation, 2009. p. 5-19. ISBN: 978-83-929922-1-9.
    Detail

    AUGUSTIN, P. Simulation of Fatigue Crack Growth in the High Speed Machined Panel under the Constant Amplitude and Spectrum Loading. In Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue. Dodrecht: Springer Science+Business Media, 2009. p. 1005-1018. ISBN: 978-90-481-2745-0.
    Detail

  • 2007

    AUGUSTIN, P. Analysis of Fatigue Crack Growth under the Spectrum Loading. Letecký zpravodaj, 2007, vol. 2007, no. 3, p. 18 ( p.)ISSN: 1211- 877X.
    Detail

    AUGUSTIN, P. Prediction of Crack Growth in Integrally Stiffened Panels. Letecký zpravodaj, 2007, vol. 2007, no. 2, p. 5 ( p.)ISSN: 1211- 877X.
    Detail

  • 2006

    AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J. Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear. Letecký zpravodaj, 2006, vol. 2006, no. 3, p. 34-36. ISSN: 1211-877X.
    Detail

  • 2005

    AUGUSTIN, P.; PLHAL, M.; ŠPLÍCHAL, J. FEM Based Fatigue Life Analysis of Landing Gear. Letecký zpravodaj, 2005, vol. 2005, no. 3, p. 6 ( p.)ISSN: 1211- 877X.
    Detail

  • 2004

    KUNZ, J.; SIEGL, J.; NEDBAL, I.; AUGUSTIN, P.; PÍŠTĚK, A. Application of Quantitative Microfractography in Damage- Tolerance and Fatigue Evaluation of Wing Spar. In ICAS 2004. Yokohama: 2004. p. 564 ( p.)ISBN: 0-9533991-6- 8.
    Detail

    AUGUSTIN, P. Fatigue and Crack Propagation Calculations of Wing Spar Structure. Letecký zpravodaj, 2004, vol. 2004, no. 3, p. 12 ( p.)ISSN: 1211- 877X.
    Detail

  • 2003

    KUNZ, J.; SIEGL, J.; NEDBAL, I.; AUGUSTIN, P.; JURAČKA, J. Fraktografická rekonstrukce časového průběhu únavového porušování nosníku křídla letounu. In FRACTOGRAPHY 2003. Košice: Institute of Materials Research of the Slovak Academy of Sciences, 2003. p. 283-291. ISBN: 80-968543-2-1.
    Detail

  • 2001

    BUJNOCH, L.; AUGUSTIN, P.; LAPČÍK, L. Railway Track Mats Based On Recycled Shredded Rubber. Materiálové inžinierstvo, 2001, vol. VIII, no. 3/ 2001, p. 47 ( p.)ISSN: 1335- 0803.
    Detail

    LAPČÍK, L.; AUGUSTIN, P.; PÍŠTĚK, A.; BUJNOCH, L. Measurement of the dynamic stiffness of recycled rubber based railway track mats according to the DB-TL 918.071 standard. APPLIED ACOUSTICS, 2001, vol. 62, no. 9, p. 1123-1128. ISSN: 0003-682X.
    Detail | WWW

    AUGUSTIN, P. Damage Tolerance Evaluation of the Wing Spar with Cracked Web. RESEARCH BULLETIN, 2001, vol. 2001, no. 11, p. 7 ( p.)ISSN: 1425- 2104.
    Detail

    BUJNOCH, L., AUGUSTIN, P., LAPČÍK, L. Railway track mats based on recycled shredded rubber. In TRANSCOM 2001 - Proceedings Section 5. Žilina: University of Žilina, 2001. p. 155 ( p.)ISBN: 80-7100-850- 8.
    Detail

  • 2000

    AUGUSTIN, P.; JURAČKA, J. FEM MODEL OF COMPOSITE WING VERSUS EXPERIMENTAL MEASUREMENT. RESEARCH BULLETIN, 2000, vol. 2000, no. Part 1, p. 139-145. ISSN: 1425-2104.
    Detail

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