Ing.

Tomáš Katrňák

FSI, LÚ OLT – asistent

+420 54114 2231
katrnak@fme.vutbr.cz

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Ing. Tomáš Katrňák

Publikace

  • 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, roč. 27, č. 1, s. 6-14. ISSN: 1335-2393.
    Detail | WWW

  • 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, roč. 21, č. 4, s. 112-121. ISSN: 2083-4799.
    Detail | WWW

  • 2020

    KATRŇÁK, T.; JURAČKA, J.; JEBÁČEK, I. Research of Effects of Defects on Stability Failures of Semi-monocoque Stiffeners. AVIATION, 2020, roč. 23, č. 3, s. 83-90. ISSN: 1648-7788.
    Detail | WWW | 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 2014. 1. Conference Engineering Mechanics 2018, Svratka, ČR: ACAD SCI CZECH REPUBLIC, INST THEORETICAL & APPLIED MECHANICS, PROSECKA 76, PRAGUE 9, 190 00, CZECH REPUBLIC, 2018. s. 373-376. ISBN: 978-80-86246-91-8. ISSN: 1805-8248.
    Detail | WWW

    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. s. 171-175. ISBN: 978-0-8153-7602-6.
    Detail | WWW

  • 2017

    KATRŇÁK, T.; JURAČKA, J. Topometry FEM optimization of the wing structure of the transport aircraft. AVIATION, 2017, roč. 2017, č. 21, s. 29-34. ISSN: 1648-7788.
    Detail | WWW

    KATRŇÁK, T. Design of new parameters for evaluation of load capacity of semi-shell structures. In Engineering Mechanics 2017. Engineering mechanics 2014. 1. konference Engineering Mechanics 2017, Svratka, ČR: Brno University of Technology, 2017. s. 442-445. ISBN: 978-80-214-5497-2. ISSN: 1805-8248.
    Detail | WWW

  • 2016

    KATRŇÁK, T.; AUGUSTIN, P.; VLČEK, D. Fatigue analyses and optimization of L 410 NG aircraft. Letecký zpravodaj, 2016, roč. 2016, č. 2, s. 39-41. ISSN: 1211-877X.
    Detail | WWW

  • 2015

    KATRŇÁK, T.; JURAČKA, J. Detailed topometry FEM optimization of wing structural panel. Applied Mechanics and Materials, 2015, roč. 821, č. 821, s. 357-363. ISSN: 1662- 7482.
    Detail | WWW

    KATRŇÁK, T.; JURAČKA, J.; SYMONOV, V. Structural analyses of small transport aircraft by the Institute of Aerospace Engineering. Letecký zpravodaj, 2015, roč. 2015, č. 3, s. 21-23. ISSN: 1211-877X.
    Detail | WWW

  • 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. s. 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, roč. 2012, č. 22, s. 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. s. 189-192. ISBN: 978-80-7043-597- 7.
    Detail

*) Citace publikací se generují jednou za 24 hodin.