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
Drag Coefficient in Level Flight Formulas
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. And is denoted by C
D
.
Formulas to find Drag Coefficient in Level Flight
f
x
Coefficient of Drag for given Thrust-to-Weight Ratio
Go
f
x
Coefficient of Drag for given Thrust and Weight
Go
Level Flight formulas that make use of Drag Coefficient
f
x
Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
Go
f
x
Coefficient of Lift for given Thrust-to-Weight Ratio
Go
f
x
Coefficient of Lift for given thrust and weight
Go
f
x
Thrust of Aircraft required for Level, Unaccelerated Flight
Go
f
x
Thrust-to-weight ratio
Go
f
x
Thrust for given coefficients of lift and drag
Go
f
x
Weight of Aircraft for given Coefficients of Lift and Drag
Go
f
x
Power required for given aerodynamic coefficients
Go
f
x
Weight of aircraft for given required power
Go
List of variables in Level Flight formulas
f
x
Lift Coefficient
Go
f
x
Thrust-to-Weight Ratio
Go
f
x
Thrust
Go
f
x
Weight of Body
Go
FAQ
What is the Drag Coefficient?
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Can the Drag Coefficient be negative?
{YesorNo}, the Drag Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!