Obliczenia flatteru prostokątnego płata ze sterem za pomocą MSC NASTRAN, ZONA ZAERO i ANSYS/Fluent - porównanie z wynikami badań w tunelu aerodynamicznym

@article{Chajec2016ObliczeniaFP,
  title={Obliczenia flatteru prostokątnego płata ze sterem za pomocą MSC NASTRAN, ZONA ZAERO i ANSYS/Fluent - por{\'o}wnanie z wynikami badań w tunelu aerodynamicznym},
  author={W. Chajec and Adam Dziubiński},
  journal={Transactions of the Institute of Aviation},
  year={2016},
  volume={243},
  pages={53-72}
}
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2 Citations

2 Citations

Separation safety analysis using CFD simulation and remeshing

Comparison of flutter calculation methods based on ground vibration test result

  • W. Chajec
  • Engineering
    Aircraft Engineering and Aerospace Technology
  • 2019
A low-cost but credible method of low-subsonic flutter analysis based on ground vibration test (GVT) results is presented and results in comparison with the outcome obtained by means of the more credible software are presented.