FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Aircraft Mechanics
Thrust Coefficient in Conceptual Design Formulas
Thrust Coefficient is the ratio of actual thrust to the ideal thrust. And is denoted by C
T
.
Conceptual Design formulas that make use of Thrust Coefficient
f
x
Average Blade Lift Coefficient
Go
FAQ
What is the Thrust Coefficient?
Thrust Coefficient is the ratio of actual thrust to the ideal thrust.
Can the Thrust Coefficient be negative?
{YesorNo}, the Thrust Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!