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

DOI

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.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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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  - 10.2991/mecs-17.2017.75
ID  - Li2016/06
ER  -