buck_justice wrote:So, are they effective on the Pacer? Does it really benefit from the generators?
Does MicroVG use the small or the large generators on the wing and tail?
Is the placement the same as on the Cessna 172?
I was first introduced to VGs 31 years ago when an AD came out for Aerostars. In certain flight configurations the wing would not stall but the rudder and elevators would. Pipers fix was the water rudder(abomination to that airplane) and Machen's is VGs on the vertical stabilizer and under the horizontal stabilizer. The Aerostar that we acquired at the time had the water rudder . We did not have it 90 days and it was removed for the Machen solution. Did we gain more authority in the rudder and elevator compaired to pre AD? Yes we did. So far i have given two examples of two completely different mission airplanes . Will you feel them take effect 10 miles over the stall speed, not at all. For GA purposes they are an enhancement to the characteristics of slow flight close to stall.
Your pacer has a different wing than the 172 which would probably require a different placement.
And young guys, this is an old guy preaching a bit: rudder is what will bring the down wing up smartly when slow. Aileron authority, not me. I will use the rudder first and foremost to get the down wing up smartly. Dutch Rolls to 45 degrees will make you believe in rudder authority. If you don't lead rudder bringing the wing up, it will be dragged back by adverse yaw and the nose will come off target. Vgs will not replace the need for aggressive rudder.
If Vgs get pilots to land slower, I am for them. If they get pilots to emphasize aileron over rudder and takeoff at scary pitch attitude, I am against them.
Agreed, I am not saying not use to use the rudder and especially at low speeds.