I did some engine-out flight testing the other day and thought I'd share my results FWIW. My airplane is an O235-L2C Long-EZ with high-compression pistons, a Hertzler propeller, wheel pants, and gear leg fairings. Gross weight was about 1200 pounds. I climbed to 14,500 and stayed within about 10 miles of the airport (1424 MSL).
With the ignition and fuel off, I found that the prop would windmill down to 70KIAS. As I lowered the nose, it would "tick over" occasionally at 85 - 90 KIAS but not enough to start the engine. It was necessary to attain 110 KIAS before the engine started. This surprised me as I had been led to believe by the pundits that it would take considerably more airspeed.
With a windmilling prop the rate of descent was 800 - 900 fpm at about 80 KIAS. After I stopped the prop and set up a a 75 KIAS glide, the rate of descent was slightly less at 700 - 800 fpm. The pitch attitude was a mild 3 - 5 degrees nose low. With full aft stick the airplane indicated 51 KIAS and about 500 feet per minute rate of descent -- very similar to what I've seen at idle thrust.
Regrettably, I didn't take the time at altitude to lower the nosegear and landing brake to note the additional descent rate. And when I lowered them for the landing, I was too busy to take notes :-) All in all, I spent about 15 minutes from engine shutdown to touchdown which equates to an 866 fpm average descent rate and agrees with what I saw on the VSI. My groundtrack covered about 25 NM, although I could easily have stretched that if I had maintained the optimum airspeed and not turned so much.
Next time (although I'm not sure there will be a "next time") I would use a voice recorder to log airspeeds, rates of descent, etc. Writing on my clipboard was a poor way to go. Also, I'd probably restart the engine at low key and use idle power for the remainder; the performance difference isn't worth the additional risk IMO.