The name of the thread of course describes an oversimplification in classification. The terms were stated to me in response to a question and I had not heard it before concerning aircraft handling at either end of the spectrum between aircraft high glide ratios and high sink rates. I could change the title to those terms but the discussion would be the same. The qualities I found in the glide ratios and sink rate differences on the few planes I have owned and flown vary greatly and particular combinations of those qualities are generally pointed to as "the reason pilots either love or hate a Maule". (Quote is from Budd Davisson).
In my own limited experience, management of power in the normal landing changes immensely from one end of this spectrum, (high glide ratio) aircraft to the other, (high sink rate). My experience ranges at either end from no more than a hundred hours in PA 18 to three times that in the CH 701. In earlier posts by a 701 builder I was asked to describe the details of normal take off and landing for that aircraft and they were of help to the pilot/builder. Knowing that particular quality of the aircraft before hand is a very important thing. It saves quashing the gear in a surprise attack from gravity.
With the PA-18, the wing continued to glide long after the power was cut and I found different pilot technique was required to reduce it to stall either by speed changes in approach speed or flaps and had I continued learning techniques for that plane I would have mastered dumping flaps to make touchdown point. It just wants to keep flying. In the 701, with high sink rate, I managed much less for the wing and much more by throttle adjustment at landing, hardly ever using flaps. That wing will stop flying in flare with no more than closing throttle. Most planes flown by pilots on this board will fall in between these two extremes for the two qualities of glide and sink that seem to be on opposite ends of the range of lift. I had hoped to speak to those design differences by eliminating the pilot experience difference as much as possible. Of course either of these aircraft can perform in a given situation with adjustment by the pilot. I wanted to point to the reason for those adjustments from the point of view of design. I thought it to be a worthwhile discussion and useful for those with less experience. My bad?
