Proceedings of the 2017 2nd International Conference on Machinery, Electronics and Control Simulation (MECS 2017)

The Study of Air Flow for Uniform Profile Numerical Simulation and Influence Factors

Authors
XinLei Li
Corresponding Author
XinLei Li
Available Online June 2016.
DOI
https://doi.org/10.2991/mecs-17.2017.75How to use a DOI?
Keywords
Airfoil profile, boundary layer, flow around, numerical simulation
Abstract
This article use Fluent to make numerical simulation of air flow for uniform and around airfoil profile. By changing different angle of attacks and different profile shapes, I analyze the distribution of pressure velocity and temperature field around profile to further evident the application value of boundary layer theory.
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This is an open access article distributed under the CC BY-NC license.

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Volume Title
Proceedings of the 2017 2nd International Conference on Machinery, Electronics and Control Simulation (MECS 2017)
Series
Advances in Engineering Research
Publication Date
June 2016
ISBN
978-94-6252-352-4
ISSN
2352-5401
DOI
https://doi.org/10.2991/mecs-17.2017.75How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - XinLei Li
PY  - 2016/06
DA  - 2016/06
TI  - The Study of Air Flow for Uniform Profile Numerical Simulation and Influence Factors
BT  - Proceedings of the 2017 2nd International Conference on Machinery, Electronics and Control Simulation (MECS 2017)
PB  - Atlantis Press
SN  - 2352-5401
UR  - https://doi.org/10.2991/mecs-17.2017.75
DO  - https://doi.org/10.2991/mecs-17.2017.75
ID  - Li2016/06
ER  -