True, true. The increase drag (frction) due to the increase in the Angle of attack of the aircraft necesary to maintain the the alt.
Prolly one dozen of one and a half of the other, but, if the
angle of attack were fixed as wel as the alt and the thrust, and the weithgt were added in such a way that drag profile was
not changed, (internally), I would say the plane would slow,
in accordance w the E equation. (increasing M would
reduce V for all values M>0 until V=0).
But since I didnt have the E equation proior to this debate
NOR did expect anybody else to have it, I can only say that
this is my humble, yet correct, opinion
