Engine off glide tests with acro wing tips from approx. 7,000 ft to 4,000 ft was done engine off, cowl flaps closed at 50, 60, & 70 kts IAS. At 51 kts ave.: L/D = 15.5:1, -333 fpm descent, 60 kts L/D = 14.8:1, -411 fpm, 70 kts L/D: 13.3:1, 530 fpm descent.
I now need to do glide tests around the best so I will test at 45 kts and 55 kts.