Basic Principles of Vortex Generators
Introduction to Vortex Generators
Vortex generators (VGs) are aerodynamic devices that have become
increasingly important in various engineering applications. These
devices are designed to modify the behavior of fluid flow by generating
controlled vortices, which can significantly impact the performance of
aerodynamic systems.
Key Concept: Vortex generators create coherent
turbulent structures that energize the boundary layer, thereby delaying
flow separation and improving aerodynamic efficiency.
Boundary Layer Theory
The boundary layer concept, first introduced by Ludwig Prandtl in 1904,
is fundamental to understanding vortex generator operation. It describes
the region where:
Figure 1: Boundary layer development and velocity profile over a flat
plate
δ(x) = 5.0 × √(νx/U∞)
where δ is boundary layer thickness, x is distance from leading edge,
ν is kinematic viscosity, and U∞ is free stream velocity
Flow Regime |
Reynolds Number (Re) |
Characteristics |
Laminar |
Re < 5 × 10⁵ |
Smooth, layered flow |
Transitional |
5 × 10⁵ < Re < 10⁶ |
Mixed flow characteristics |
Turbulent |
Re > 10⁶ |
Chaotic, mixing flow |
Vortex Generation Mechanisms
Figure 2: Vortex formation process behind a vortex generator
Key Parameters Affecting Vortex Formation
Geometric Parameters
- Height (h): 0.8δ - 1.2δ
- Length (l): 1.5h - 2.5h
- Angle of incidence (β): 15° - 25°
- Spacing (s): 3h - 7h
Flow Parameters
- Reynolds number (Re)
- Mach number (M)
- Pressure gradient (dp/dx)
- Boundary layer thickness (δ)
Performance Metrics and Analysis
Figure 3: Relationship between vortex generator height and performance
improvement
ΔCL/CD = f(h/δ, β, Re)
Relationship between lift-to-drag ratio improvement and key
parameters
Performance Metric |
Typical Improvement Range |
Optimization Parameter |
Maximum Lift Coefficient |
10-15% |
Height ratio (h/δ) |
Stall Angle |
2-4 degrees |
Angle of incidence (β) |
Drag Reduction |
5-8% |
Spacing ratio (s/h) |
References
-
Lin, J.C., "Review of research on low-profile vortex generators to
control boundary-layer separation," Progress in Aerospace Sciences,
Vol. 38, No. 4-5, 2002, pp. 389-420.
-
Godard, G., and Stanislas, M., "Control of a decelerating boundary
layer," Aerospace Science and Technology, Vol. 10, No. 3, 2006, pp.
181-191.
-
Ashill, P.R., Fulker, J.L., and Hackett, K.C., "Research at DERA on
sub boundary layer vortex generators (SBVGs)," AIAA Paper 2001-0887,
2001.
-
Pauley, W.R., and Eaton, J.K., "Experimental study of the development
of longitudinal vortex pairs embedded in a turbulent boundary layer,"
AIAA Journal, Vol. 26, No. 7, 1988, pp. 816-823.