I added vortex generators & stall strips similar to Jim and my results are similar too;
I have 3/8" x 6" stall strips just above the leading edge of the center wing section airfoil. These are mounted with the outer end directly behind the propeller tip, as called out in the T-18 news letters.
The vortex generators I made were copies of the 'Hall' type.
http://www.hallwindmeter.com/vortex.php I bent them up out of aluminum and stuck them on the wing with double sticky carpet tape. (use wax remover on paint first, or they will fall off)
I used 2 each per wing, in front of the ailerons. The first is 2" outboard of the outer wing panel attach join, the second 12'' outboard of the first. (I presume there is some outward span-wise flow in low speed flight.)
They are 10% back from the leading edge, measured over the skin.
The effect: The stall strips behave exactly as the news letters said, a testimony to the data they contain. The stall speed is not reduced by these strips, they simply warn the pilot with a nice stick shake about 3-5 MPH above stall speed. The vortex generators increase the effectiveness of the ailerons in the stall.
The vortex generators did not reduce the top speed of my aircraft by any amount that I could notice.
They do make low speed flight much more comfortable for me.