Publikační výsledky

• 2023

  KUBIT, A.; ZIELECKI, W.; BEREZOWSKI, W.; PERŁOWSKI, R.; ŁABNO, K.; KATRŇÁK, T. Experimental Study of the Impact of Notches Made in the Front Edge of Adherends on the Properties of Static and Fatigue Strength of Adhesive Joints. Acta Mechanica Slovaca, 2023, vol. 27, no. 1, p. 6-14. ISSN: 1335-2393.
  Detail

• 2021

  ZIELECKI, W.; BURNAT, K.; KUBIT, A.; KATRŇÁK, T. Effect of Holes in Overlap on the Load Capacity of the Single-Lap Adhesive Joints Made of EN AW-2024-T3 Aluminium Alloy. Advances in Materials Science, 2021, vol. 21, no. 4, p. 112-121. ISSN: 2083-4799.
  Detail

• 2020

  KATRŇÁK, T.; JURAČKA, J.; JEBÁČEK, I. Research of Effects of Defects on Stability Failures of Semi-monocoque Stiffeners. Aviation, 2020, vol. 23, no. 3, p. 83-90. ISSN: 1648-7788.
  Detail | Plný text v Digitální knihovně

• 2018

  KATRŇÁK, T.; JURAČKA, J. Buckling analyses of compressed stiffener with finite element methods. In ENGINEERING MECHANICS 2018 - Book of full texts. Engineering Mechanics. 1. Conference Engineering Mechanics 2018, Svratka, ČR: ACAD SCI CZECH REPUBLIC, INST THEORETICAL & APPLIED MECHANICS, PROSECKA 76, PRAGUE 9, 190 00, CZECH REPUBLIC, 2018. no. 1, p. 373-376. ISBN: 978-80-86246-91-8. ISSN: 1805-8248.
  Detail

  KATRŇÁK, T. A combined parameter for graphic evaluation of the load capacity of fuselage. In New Trends in Civil Aviation. 1. London, UK: CRC Press, 2018. p. 171-175. ISBN: 978-0-8153-7602-6.
  Detail

• 2017

  KATRŇÁK, T.; JURAČKA, J. Topometry FEM optimization of the wing structure of the transport aircraft. Aviation, 2017, vol. 2017, no. 21, p. 29-34. ISSN: 1648-7788.
  Detail

  KATRŇÁK, T. Design of new parameters for evaluation of load capacity of semi-shell structures. In Engineering Mechanics 2017. Engineering Mechanics. 1. konference Engineering Mechanics 2017, Svratka, ČR: Brno University of Technology, 2017. no. 1, p. 442-445. ISBN: 978-80-214-5497-2. ISSN: 1805-8248.
  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

• 2015

  KATRŇÁK, T.; JURAČKA, J. Detailed topometry FEM optimization of wing structural panel. Applied Mechanics and Materials, 2015, vol. 821, no. 821, p. 357-363. ISSN: 1662-7482.
  Detail

  KATRŇÁK, T.; JURAČKA, J.; SYMONOV, V. Structural analyses of small transport aircraft by the Institute of Aerospace Engineering. Letecký zpravodaj, 2015, vol. 2015, no. 3, p. 21-23. ISSN: 1211-877X.
  Detail

• 2013

  SYMONOV, V.; KATRŇÁK, T. FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure. In New Trends in Civil Aviation 2013. 1. Brno: Akademické nakladatelství CERM Brno, 2013. p. 90-92. ISBN: 978-80-7204-843-4.
  Detail

• 2012

  KATRŇÁK, T.; PLHAL, M. SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY. RESEARCH BULLETIN, 2012, vol. 2012, no. 22, p. 1-8. ISSN: 1425-2104.
  Detail

• 2007

  PEŠÁK, M.; KATRŇÁK, T. OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING-EXPERIMENTAL VERIFICATION. In Proceedings-5th International PhD Conference on Mechanical Engineering PhD 2007. 2007. Plzeň: Západočeská univerzita v Plzni, 2007. p. 189-192. ISBN: 978-80-7043-597-7.
  Detail

*) Citace se generují jednou za 24 hodin.