Minimum Thrust required when lift to drag is maximum. It’s directly proportional to the aircraft weight. Its SI unit is Newton.
Where W= weight
k= induced drag factor
Cd0= zero-lift drag coefficient
Minimum Thrust Required Calculator by Mohit Kudal
- Post author:mohitkudal
- Post published:February 20, 2021
- Post category:Aerospace Calculator / Airplane Performance Calculator / Engineering Calculator / Flight Mechanics Calculator / General Calculator