Moment Coefficient Formula

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The Moment Coefficient is divided by the dynamic pressure, the area and the chord of the airfoil, the result is known as the pitching moment coefficient. Check FAQs
Cm=MtqALc
Cm - Moment Coefficient?Mt - Moment?q - Dynamic Pressure?A - Area For Flow?Lc - Chord Length?

Moment Coefficient Example

With values
With units
Only example

Here is how the Moment Coefficient equation looks like with Values.

Here is how the Moment Coefficient equation looks like with Units.

Here is how the Moment Coefficient equation looks like.

0.0311Edit=59Edit10Edit50Edit3.8Edit
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Moment Coefficient Solution

Follow our step by step solution on how to calculate Moment Coefficient?

FIRST Step Consider the formula
Cm=MtqALc
Next Step Substitute values of Variables
Cm=59N*m10Pa503.8m
Next Step Convert Units
Cm=59J10Pa503.8m
Next Step Prepare to Evaluate
Cm=5910503.8
Next Step Evaluate
Cm=0.0310526315789474
LAST Step Rounding Answer
Cm=0.0311

Moment Coefficient Formula Elements

Variables
Moment Coefficient
The Moment Coefficient is divided by the dynamic pressure, the area and the chord of the airfoil, the result is known as the pitching moment coefficient.
Symbol: Cm
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Moment
Moment is an overturning effect (tends to bend or turn the member) created by the force(load) acting on a structural member.
Symbol: Mt
Measurement: EnergyUnit: N*m
Note: Value can be positive or negative.
Dynamic Pressure
Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Symbol: q
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
Area For Flow
Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.
Symbol: A
Measurement: AreaUnit:
Note: Value should be greater than 0.
Chord Length
Chord Length is the length of a line segment connecting any two points on the circumference of a circle.
Symbol: Lc
Measurement: LengthUnit: m
Note: Value should be greater than 0.

Other formulas in Hypersonic Flow Parameters category

​Go Axial Force Coefficient
μ=FqA
​Go Coefficient of Drag
CD=FDqA
​Go Coefficient of Pressure with Similarity Parameters
Cp=2θ2(Y+14+(Y+14)2+1K2)
​Go Deflection Angle
θd=2Y-1(1M1-1M2)

How to Evaluate Moment Coefficient?

Moment Coefficient evaluator uses Moment Coefficient = Moment/(Dynamic Pressure*Area For Flow*Chord Length) to evaluate the Moment Coefficient, Moment Coefficient formula is defined as a dimensionless quantity used to describe the characteristics of hypersonic flow, providing a measure of the momentum of a fluid in relation to its mass flow rate and cross-sectional area. Moment Coefficient is denoted by Cm symbol.

How to evaluate Moment Coefficient using this online evaluator? To use this online evaluator for Moment Coefficient, enter Moment (Mt), Dynamic Pressure (q), Area For Flow (A) & Chord Length (Lc) and hit the calculate button.

FAQs on Moment Coefficient

What is the formula to find Moment Coefficient?
The formula of Moment Coefficient is expressed as Moment Coefficient = Moment/(Dynamic Pressure*Area For Flow*Chord Length). Here is an example- 0.031053 = 59/(10*50*3.8).
How to calculate Moment Coefficient?
With Moment (Mt), Dynamic Pressure (q), Area For Flow (A) & Chord Length (Lc) we can find Moment Coefficient using the formula - Moment Coefficient = Moment/(Dynamic Pressure*Area For Flow*Chord Length).
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