Computation of Vibration Response of Aircraft Due to the Gap Between the Track and Roller in the Flap Subjected to Unsteady Flow

Bohan Sun, Xiaoliang Wang, Zhefeng Yu

Open source

DOI: 10.1155/ijae/5539075
Published: 2025
Container: International Journal of Aerospace Engineering
Publisher: Not recorded
Open access: yes

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Cite this work

BibTeX

@article{allodium:10.1155/ijae/5539075,
  title = {Computation of Vibration Response of Aircraft Due to the Gap Between the Track and Roller in the Flap Subjected to Unsteady Flow},
  author = {Bohan Sun and Xiaoliang Wang and Zhefeng Yu},
  year = {2025},
  journal = {International Journal of Aerospace Engineering},
  doi = {10.1155/ijae/5539075},
  url = {https://doi.org/10.1155/ijae/5539075}
}

RIS

TY  - JOUR
TI  - Computation of Vibration Response of Aircraft Due to the Gap Between the Track and Roller in the Flap Subjected to Unsteady Flow
AU  - Bohan Sun
AU  - Xiaoliang Wang
AU  - Zhefeng Yu
PY  - 2025
JO  - International Journal of Aerospace Engineering
DO  - 10.1155/ijae/5539075
UR  - https://doi.org/10.1155/ijae/5539075
ER  -

APA

Sun, B., Wang, X., & Yu, Z. (2025). Computation of Vibration Response of Aircraft Due to the Gap Between the Track and Roller in the Flap Subjected to Unsteady Flow. International Journal of Aerospace Engineering. https://doi.org/10.1155/ijae/5539075

Source records

doaj · retrieved 2026-09-25T01:31:23.582Z