Numerical Simulation of a Low Reynolds Number Airfoil
2013
In this paper, a low Reynolds number airfoil (S1223) is the objective of the study. The Navier-Stokes equations were established to simulate the complex flow around a low Reynolds number airfoil, in which the turbulence model was used. The complex flow around the airfoil was simulated at 2x105 Reynolds number and its aerodynamic characteristics were analyzed. The relationship among lift coefficient, drag coefficient and angle of attack was studied.
Keywords:
- Drag divergence Mach number
- Classical mechanics
- Control engineering
- Aerodynamic center
- Reynolds decomposition
- Reynolds equation
- Drag equation
- Engineering
- Drag coefficient
- Reynolds stress equation model
- Airfoil
- Lift coefficient
- Structural engineering
- Reynolds-averaged Navier–Stokes equations
- Reynolds number
- Mechanics
- Correction
- Source
- Cite
- Save
- Machine Reading By IdeaReader
6
References
1
Citations
NaN
KQI