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.
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• 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.
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• 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.
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  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.
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• 2009

  JURAČKA, J.; AUGUSTIN, P.; KOULA, V. Zkoušky únavového chování segmentu křídla. Transfer, 2009, vol. 2009, no. 9, p. 33-45. ISSN: 1801- 9315.
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  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.
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  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.
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  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.
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• 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.
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  AUGUSTIN, P. Prediction of Crack Growth in Integrally Stiffened Panels. Letecký zpravodaj, 2007, vol. 2007, no. 2, p. 5 ( p.)ISSN: 1211- 877X.
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• 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.
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• 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.
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• 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.
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  AUGUSTIN, P. Fatigue and Crack Propagation Calculations of Wing Spar Structure. Letecký zpravodaj, 2004, vol. 2004, no. 3, p. 12 ( p.)ISSN: 1211- 877X.
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• 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.
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• 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.
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  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.
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  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.
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• 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.
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