Recent experimental investigations conducted on Air Jet Vortex Generators (AJVG) featuring a smoothly increasing injection width produced promising results when the device was used to reduce the magnitude of flow separation about an airfoil. Testing was conducted at a Reynolds number of 6.5 × 105 on a NACA 6 series airfoil equipped with an array of the devices. The injection width monotonically increased once by a magnitude of e over the length of the device, which was tested with two main groups of blowing profiles. One set of blowing profiles featured an injection velocity that monotonically increased once by a magnitude of e. The other set of blowing profiles had an injection velocity that was constant. The exponential blowing profiles consumed less energy to produce incremental gains in lift coefficient between 0.023-0.18 when compared to the blowing profiles featuring a constant injection velocity. A 14% reduction in energy consumption was noted for a 0.16 incremental gain in lift coefficient. The current work experimentally determines the performance of the same AJVG under conditions where the boundary layer was artificially tripped to mimic the turbulence associated with operations at elevated Reynolds numbers.