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Vyhledávání Vyhledat Zavřít
Ing.
Ph.D.
FSI, LÚ OLT – odborný asistent
+420 54114 2223Jan.Navratil@vutbr.cz
Odeslat VUT zprávu
2026
HOSTINSKÝ, V.; SODJA, J.; JEBÁČEK, I.; NAVRÁTIL, J. Limits of analytical models of sandwich structures for optimization. Composite structures, 2026, vol. 382, no. 120089, 12 p.
Článek Scopus
2025
ZIKMUND, P.; KOFLER, M.; NAVRÁTIL, J.; HRSTKA, M.; POLLÁK, J.; VAN KAMPEN, E. Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials. In 2024 New Trends in Aviation Development (NTAD). Proceedings (New Trends in Aviation Development). IEEE, 2025. p. 236-241. ISBN: 979-8-3315-2774-7. ISSN: 2836-2764.
Stať ve sborníku v databázi WoS či Scopus
ŠPLÍCHAL, J.; NAVRÁTIL, J.; JURAČKA, J. Input data determination for assessment of flutter resistance of small aircraft. Aircraft Engineering and Aerospace Technology, 2025, vol. 97, no. 7, p. 833-844. ISSN: 1748-8842.
Článek WoS
2024
PATIL, A.; NAVRÁTIL, J. CFD analysis of wing-propeller interaction on the NASA X-57 Maxwell aircraft wing. In 13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons. Journal of Physics: Conference Series. IOP Publishing, 2024. p. 1-8. ISSN: 1742-6596.
NAVRÁTIL, J.; HOSTINSKÝ, V.; SODJA, J. Design of morphing wing for aerodynamic performance considering the wing flexibility effects. In 13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons. Journal of Physics: Conference Series. IOP Publishing, 2024. p. 1-8. ISSN: 1742-6596.
2023
BAJER, J.; KŠICA, F.; MARCIÁN, P.; HRSTKA, M.; NAVRÁTIL, J.; HADAŠ, Z. Concept of Autonomous Self-Sensing Metamaterial Structures for Future Aircraft. In 2023 IEEE 10th International Workshop on Metrology for AeroSpace (MetroAeroSpace). Milan, Italy: IEEE, 2023. p. 424-429. ISBN: 978-1-6654-5690-6.
2020
NAVRÁTIL, J. High-fidelity static aeroelastic simulations of the common research model. In Flexible Engineering Toward Green Aircraft. Lecture Notes in Applied and Computational Mechanics. Springer, 2020. p. 49-70. ISBN: 978-3-030-36514-1. ISSN: 1613-7736.
2018
NAVRÁTIL, J.; JIRÁSEK, A.; LOFTHOUSE A. J.; SATCHELL M. Effect of Flow Parameters Variation on Flutter Boundary of Benchmark Supercritical Wing. AIAA JOURNAL, 2018, vol. 57, no. 2, p. 772-781. ISSN: 0001-1452.
NAVRÁTIL, J.; JIRÁSEK, A.; HAMLINGTON, P.; LOFTHOUSE, A. Effect of angle of attack, gas composition and reynolds number on flutter boundary of benchmark super-critical wing. In 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. Elsevier B.V., 2018. p. 1-10. ISBN: 9788897576280.
2017
NAVRÁTIL, J. Aerodynamic shape optimization of an airliner elastic wing. In 12th International Conference on Applied Mathematical Programming and Modelling (APMOD 2016). ITM Web of Conferences. Francie: EDP Sciences, 2017. no. 00006, p. 1-9. ISBN: 9781510851924. ISSN: 2271-2097.
2016
JIRÁSEK, A.; DALENBRING, M.; NAVRÁTIL, J. Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition. In 54th AIAA Aerospace Sciences Meeting. AIAA, 2016. p. 1-11. ISBN: 978-1-62410-393-3.
JIRÁSEK, A.; NAVRÁTIL, J.; DALENBRING, M. Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition. AIAA JOURNAL, 2016, vol. 0, no. 0, p. 1-8. ISSN: 0001-1452.
2014
AMOIGNON, O.; NAVRÁTIL, J.; HRADIL, J. Study of parameterizations in project CEDESA. In 52nd AIAA Aerospace Sciences Meeting. AIAA, 2014. p. 1-19. ISBN: 978-1-62410-256-1.
AMOIGNON, O.; HRADIL, J.; NAVRÁTIL, J. A numerical study of adaptive FFD in aerodynamic shape optimization. In 52nd AIAA Aerospace Sciences Meeting. AIAA, 2014. p. 1-11. ISBN: 978-1-62410-256-1.
2013
HRADIL, J.; NAVRÁTIL, J. Free-Form Deformation parameterization for aerodynamic shape optimization. In New Trends in Civil Aviation 2013. 1. Olomoučany: AKADEMICKÉ NAKLADATELSTVÍ CERM, s. r. o. Brno, 2013. p. 22-27. ISBN: 978-80-7204-843-4.
*) Citace se generují jednou za 24 hodin.