The terms “thrust coefficient of lift” are not typically used together in flight mechanics. However, I can provide you with definitions for “thrust coefficient” and “lift coefficient,” which are separate concepts in aerodynamics.
The thrust coefficient, denoted as , is a dimensionless parameter used to quantify the efficiency of a propulsion system, such as a jet engine or a propeller. It relates the thrust generated by the propulsion system to the mass flow rate of air passing through the engine.
Clt means thrust lift coefficient
Cdt means thrust drag coefficient
Cdo means zero drag coefficient
K means constant