I give up, after many, many years!
"Mxsmanic" wrote in message
...
Your increased speed will produce more lift, which will tend to raise the
aircraft, slowing the rate of descent and potentially leveling the
aircraft or
producing a climb. For any given setting of AOA and thrust, the aircraft
will
tend to converge on a specific density altitude. If AOA is held and
thrust is
increased, the aircraft will converge on a higher final altitude than it
would
if thrust were not increased. Increasing power (and thus thrust) at
constant
AOA will produce a positive change in climb rate, because it increases the
speed of air flowing over the wings.
This is much less inaccurate than your other statement.
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