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 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 Tags: Aircraft Performance, flight mechanics Read more articles Previous PostAerodynamic Efficiency Calculator by Mohit Kudal Next PostLift Force Calculator by Mohit Kudal You Might Also Like Minimum Turn Radius Calculator October 25, 2020 Lift Coefficient (with change in Angle of attack) June 5, 2021 Capture Area Ratio of Subsonic Inlet April 30, 2021