A theoretical study of serrated leading edges in aerofoil and vortical gust interaction noise

Xun Huang

Open source

DOI: 10.1186/s42774-019-0010-y
Published: 2019-02-28
Container: Advances in Aerodynamics
Publisher: Springer Science and Business Media LLC
Open access: unknown

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Cite this work

BibTeX

@article{allodium:10.1186/s42774-019-0010-y,
  title = {A theoretical study of serrated leading edges in aerofoil and vortical gust interaction noise},
  author = {Xun Huang},
  year = {2019},
  journal = {Advances in Aerodynamics},
  doi = {10.1186/s42774-019-0010-y},
  url = {https://doi.org/10.1186/s42774-019-0010-y}
}

RIS

TY  - JOUR
TI  - A theoretical study of serrated leading edges in aerofoil and vortical gust interaction noise
AU  - Xun Huang
PY  - 2019
JO  - Advances in Aerodynamics
DO  - 10.1186/s42774-019-0010-y
UR  - https://doi.org/10.1186/s42774-019-0010-y
ER  -

APA

Huang, X. (2019). A theoretical study of serrated leading edges in aerofoil and vortical gust interaction noise. Advances in Aerodynamics. https://doi.org/10.1186/s42774-019-0010-y

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crossref · retrieved 2026-11-10T12:34:36.410Z