Hello,
As if it was not yet obvious from my previous questions on the topic, I must be stupid because I cannot understand how the drag is calculated.
An example in pictures:
How can the parasitic drag be negative?
If I go back to a normal speed for this altitude:
Even at normal cruise speed, some "negative" drag is calculated and reducing the parasitic drag by half.
Could you explain this please?
I have a really hard time tuning the drag of the aircraft, and I believe the missing drag in cruise (reflected in a too low N1 in cruise) is due to this negative drag.
Thank you.