Assuming the same aircraft and same weight in unaccelerated, level flight.
If the CG is located more forward the tail needs to produce more downforce. This is the same as more weight in the tail but since lift is drag it creates mre drag that real weight. The downforce produced of the tail must be compensated by the wing with lift in the UP direction, which creates drad too since created by a higher AOA. And total weight stays the same.
Then we have to consider that the Huskys airfoil has a substantial hysteresis. The amount of lift needed for flying X can be created by a lower speed with higher AOA or higher speed at lower AOA. Thomas B. will second that in the MU2 he has. There above FL240 the sperad is 20 KTS.
Heres the effect in the real world explained.
#1
Climb with 90 mph to 6000 ft with cruise climb 25/23. As soon as you reach 6000 ft bring the power back to 2000/ 22 Level the plane and trim the plane will accelerate to 106 mph and cruise with that speed and a high AOA.
#2
Same than above but level of at 6300 ft, same trimming etc as above. When 106 mph are established, slightly trim forward, don´t touch the stick. The nose will drop slightly, speed will build up to 115mph and the nose will raise again. Do not allow the nose to raise more than level flight, which is a bit lower than position in #1. Speed will establish at 115 mph after loosing about 200ft with 200ft /min. Alt now shows 6100 and level flight at 115mph. To get to 6000ft do not touch the trim but ease the stick slightly forward. Do not let the nose come up when the extra 2 mph will be bleeding off.
Youare now flying level at the desired alt with higher speed and less AOA, untill you pull up!
Enjoy your Husky and fly safe!
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