Design Considerations for Vortex Generators
Introduction to VG Design
The design of vortex generators requires careful consideration of
multiple parameters to achieve optimal performance. The effectiveness of
VGs depends on their ability to generate coherent vortical structures
while minimizing parasitic drag.
Key Design Objectives:
- Maximize boundary layer mixing efficiency
- Minimize parasitic drag
- Ensure structural integrity
- Optimize for specific operating conditions
Design Optimization
Figure 1: Efficiency contours as a function of height ratio and angle
of incidence
η = f(h/δ, β) = ηmax × [1 - (h/δ - 1.2)²/2] × [1 - (β - 20)²/400]
Empirical correlation for VG efficiency based on geometric
parameters
Parameter |
Optimal Range |
Critical Factors |
Height Ratio (h/δ) |
0.8 - 1.2 |
Boundary layer thickness, Reynolds number |
Angle of Incidence (β) |
15° - 25° |
Flow speed, pressure gradient |
Length-to-Height Ratio |
2.0 - 3.0 |
Material constraints, manufacturing |
VG Configurations
Figure 2: Common vortex generator array configurations
Counter-rotating Arrays
- Stronger vortex interaction
- Better mixing characteristics
- Optimal spacing: 2-3h
- Preferred for high-lift applications
Co-rotating Arrays
- Lower parasitic drag
- More uniform downstream flow
- Optimal spacing: 4-5h
- Suitable for drag reduction
Material Selection and Manufacturing
Material |
Advantages |
Limitations |
Applications |
Aluminum |
Lightweight, corrosion-resistant |
Cost, formability |
Aircraft, high-performance |
Composite |
Design flexibility, weight |
Manufacturing complexity |
Wind turbines, aerospace |
Thermoplastic |
Cost-effective, mass production |
Temperature limitations |
Automotive, HVAC |
Manufacturing Considerations
- Surface finish requirements: Ra < 63 μin
- Installation tolerances: ±2° angular, ±0.5mm position
- Structural integrity: 3× design load safety factor
- Environmental resistance: UV, temperature, moisture
Analysis and Validation Methods
Computational Methods
- RANS simulations
- Large Eddy Simulation
- Grid sensitivity studies
- Turbulence model validation
Experimental Techniques
- Wind tunnel testing
- PIV measurements
- Surface flow visualization
- Force balance measurements
Performance Metrics
- Circulation strength
- Mixing efficiency
- Pressure recovery
- Total pressure loss
Γ = ∮ V⋅dl = 2πrVθ
Circulation strength calculation for vortex characterization
References
-
Anderson, B.H., et al., "A study on vortex generator design for
diffuser performance enhancement," ASME Journal of Fluids Engineering,
Vol. 143, No. 6, 2021.
-
Chen, H.C., "Optimization of vortex generator configurations using
computational fluid dynamics," Journal of Aircraft, Vol. 55, No. 6,
2018, pp. 2418-2430.
-
Wendt, B.J., "Initial circulation and peak vorticity behavior of
vortices shed from airfoil vortex generators," NASA CR-198958, 1994.
-
Taylor, H.D., "Design criteria for and applications of the vortex
generator mixing principle," United Aircraft Corporation Research
Department Report M-15038-1, 1948.