Editing Vortex generator (section)

==Aftermarket installation==
Many aircraft carry vane vortex generators from time of manufacture, but there are also aftermarket suppliers who sell VG kits to improve the [[STOL]] performance of some light aircraft.<ref name="Micro">{{cite web|url = http://www.microaero.com/|title = Micro Vortex Generators for Single and Twin Engine Aircraft|access-date = 2008-03-15|last = Micro AeroDynamics|year = 2003}}</ref>  Aftermarket suppliers claim (i) that VGs lower stall speed and reduce take-off and landing speeds, and (ii) that VGs increase the effectiveness of ailerons, elevators and rudders, thereby improving controllability and safety at low speeds.<ref>{{cite web|url=http://www.landshorter.com/page2.html |title=Land Shorter! Benefits |publisher=Landshorter.com |date= |access-date=2012-10-09}}</ref> For home-built and experimental [[homebuilt aircraft|kitplane]]s, VGs are cheap, cost-effective and can be installed quickly; but for certified aircraft installations, [[Type certificate|certification]] costs can be high, making the modification a relatively expensive process.<ref name="Micro" /><ref name="Busch"/>

Owners fit aftermarket VGs primarily to gain benefits at low speeds, but a downside is that such VGs may reduce cruise speed slightly. In tests performed on a [[Cessna 182]] and a [[Piper Cherokee|Piper PA-28-235 Cherokee]], independent reviewers have documented a loss of cruise speed of {{convert|1.5|to|2.0|kn|km/h|1|abbr=on}}.  However, these losses are relatively minor, since an aircraft wing at high speed has a small angle of attack, thereby reducing VG drag to a minimum.<ref name="Busch"/><ref name="COPAMay2003">Psutka, Kevin, ''Micro-vortex generators'', [[Canadian Owners and Pilots Association|COPA Flight]], August 2003</ref><ref name="COPAJuly2004">Kirkby, Bob, ''Vortex Generators for the Cherokee 235'', [[Canadian Owners and Pilots Association|COPA Flight]], July 2004</ref>

Owners have reported that on the ground, it can be harder to clear snow and ice from wing surfaces with VGs than from a smooth wing, but VGs are not generally prone to inflight icing as they reside within the boundary layer of airflow. VGs may also have sharp edges which can tear the fabric of airframe covers and may thus require special covers to be made.<ref name="Busch"/><ref name="COPAMay2003" /><ref name="COPAJuly2004" />

For twin-engined aircraft, manufacturers claim that VGs reduce single-engine control speed ([[V speeds|Vmca]]), increase zero fuel and gross weight, improve the effectiveness of ailerons and rudder, provide a smoother ride in turbulence and make the aircraft a more stable instrument platform.<ref name="Micro" />