Publikační výsledky

• 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). 2024 New Trends in Aviation Development (NTAD). IEEE, 2025. p. 236-241. ISBN: 979-8-3315-2774-7. ISSN: 2836-2764.
  Detail

  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.
  Detail

• 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.
  Detail

  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.
  Detail

• 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.
  Detail

• 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.
  Detail

• 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.
  Detail

  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.
  Detail

• 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.
  Detail

• 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.
  Detail

  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.
  Detail

• 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.
  Detail

  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.
  Detail

• 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.
  Detail

*) Citace se generují jednou za 24 hodin.