Vehicle aerodynamic improvement apparatus and system

1. An apparatus for improving aerodynamics of a vehicle, the apparatus comprising:

a plurality of stiffeners offset from each other;

a first airfoil configured with a thin-form sheet having a curved shape with a substantially similar arc length for an outboard surface or an inboard surface of the first airfoil;

a second airfoil coupled to the first airfoil using the plurality of stiffeners, wherein a trailing edge of the first airfoil overlaps a leading edge of the second airfoil;

an airflow inlet defined by a leading edge of the first airfoil and a pair of adjacent stiffeners of the plurality of stiffeners; and

an airflow outlet defined by the trailing edge of the first airfoil, the leading edge of the second airfoil, and he pair of stiffeners.

2. The apparatus of claim 1 , further comprising a hinge unit coupled to the inboard surface of the first airfoil and configured to mount to an external surface of the vehicle.

3. The apparatus of claim 1 , wherein the second airfoil is configured to be partially overlapped by the first airfoil to reduce airflow separation from the first airfoil.

4. The apparatus of claim 1 , further comprising a locking rod configured to attach to a door of the vehicle for auto deploying and retracting of the apparatus.

5. The apparatus of claim 1 , wherein the second airfoil is configured as a stabilizer.

6. A system for improving aerodynamics of a vehicle, the system comprising:

first and second aerodynamic units, each aerodynamic unit including a first airfoil configured with a thin-form sheet and a second airfoil interconnected to the first airfoil using a plurality of stiffeners, wherein a trailing edge of the first airfoil overlaps a leading edge of the second airfoil, wherein the first and second aerodynamic units are configured to mount to side surfaces of the vehicle; and

a third aerodynamic unit configured to mount to a top surface of the vehicle, wherein the third aerodynamic unit extends beyond a boundary region and into a region of the general airflow.

7. The system of claim 6 , wherein each aerodynamic unit further includes:

an airflow inlet defined by a leading edge of the first airfoil and a pair of adjacent stiffeners of the plurality of stiffeners; and

an airflow outlet defined by the trailing edge of the first airfoil, the leading edge of the second airfoil, and the pair of adjacent stiffeners.

8. The system of claim 6 , wherein the third aerodynamic unit is mounted substantially perpendicular to general airflow surrounding the vehicle.

9. The system of claim 6 , wherein a radius of curvature of the third aerodynamic unit is configured to be approximately between 1 and 1.75 inches.