I just watched an old video from "Flying" magazine in which Barry Schiff talked about engine-out emergencies. "Best glide speed" is an indicated airspeed (or calibrated, if you're fussy). It assumes zero wind (very seldom the actual situation), and maximum gross weight. Schiff went through a series of flight tests to determine best glide speed for a 182 (70 knots). He pulled the throttle to idle at 4500' MSL, established a stable glide at a particular speed (I don't understand how some people can make the ASI appear to be broken, "stuck at" some particular speed), and used a stopwatch to time the descent from 4000' MSL to 3000'. Then with a quick conversion to TAS and some more math, he determined the glide ratio (12:1 for a stock 182 with the prop windmilling). Do this for several indicated airspeeds, and you can bracket the best glide speed.KS170A wrote:I think if properly installed, it would give you a good sense of your true best glide speed, which some day may help make a better glide should a glide be required. I like the benefit of knowing what the optimal angle of attack is regardless of weight, but I find it more beneficial in higher-performance aircraft.....
For aircraft weights below maximum gross, which should be the case for any engine-out emergency at altitude, he used the simple formula of reducing the best glide speed by 5% for every 10% below maximum gross weight.
He also talked about the "minimum sink" speed, for when you're already over the emergency landing field, but not yet down to pattern altitude. For that, he uses something halfway between best glide and stall speed, as a rule of thumb.
He went on to demonstrate the improvement in glide ratio with the prop set to high pitch, and again with the prop stopped. Both made significant improvement in glide speeds, up to 20% with the prop stopped (assuming you've got time for that).
These experiments are all easy to do. All you need is a little math, a stopwatch, and a pilot who can make the gauges sit up and beg.
