Pitching moment Formula

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Pitching Moment is the moment acting on the airplane about its pitch axis. Check FAQs
𝑴=CmqS𝓁
𝑴 - Pitching Moment?Cm - Pitching Moment Coefficient?q - Dynamic Pressure?S - Reference Area?𝓁 - Characteristic Length?

Pitching moment Example

With values
With units
Only example

Here is how the Pitching moment equation looks like with Values.

Here is how the Pitching moment equation looks like with Units.

Here is how the Pitching moment equation looks like.

17.9832Edit=0.59Edit10Edit5.08Edit0.6Edit
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Pitching moment Solution

Follow our step by step solution on how to calculate Pitching moment?

FIRST Step Consider the formula
𝑴=CmqS𝓁
Next Step Substitute values of Variables
𝑴=0.5910Pa5.080.6m
Next Step Prepare to Evaluate
𝑴=0.59105.080.6
LAST Step Evaluate
𝑴=17.9832N*m

Pitching moment Formula Elements

Variables
Pitching Moment
Pitching Moment is the moment acting on the airplane about its pitch axis.
Symbol: 𝑴
Measurement: Moment of ForceUnit: N*m
Note: Value can be positive or negative.
Pitching Moment Coefficient
Pitching Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane pitch axis.
Symbol: Cm
Measurement: NAUnit: Unitless
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.
Reference Area
The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.
Symbol: S
Measurement: AreaUnit:
Note: Value should be greater than 0.
Characteristic Length
Characteristic Length (used in aerodynamics) is a reference length characteristic of the object under consideration.
Symbol: 𝓁
Measurement: LengthUnit: m
Note: Value should be greater than 0.

Other formulas in Aircraft Dynamics Nomenclature category

​Go Aerodynamic Axial Force
X=CxqS
​Go Aerodynamic Side Force
Y=CyqS
​Go Aerodynamic Normal Force
Z=CzqS
​Go Side force coefficient
Cy=YqS

How to Evaluate Pitching moment?

Pitching moment evaluator uses Pitching Moment = Pitching Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length to evaluate the Pitching Moment, The pitching moment is a measure of the turning force around a pitch axis, typically used to describe the rotational motion of an object, such as an aircraft or a ship, and is critical in understanding the stability and control of the vehicle, it is an essential concept in aerodynamics and naval architecture. Pitching Moment is denoted by 𝑴 symbol.

How to evaluate Pitching moment using this online evaluator? To use this online evaluator for Pitching moment, enter Pitching Moment Coefficient (Cm), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁) and hit the calculate button.

FAQs on Pitching moment

What is the formula to find Pitching moment?
The formula of Pitching moment is expressed as Pitching Moment = Pitching Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length. Here is an example- 17.9832 = 0.59*10*5.08*0.6.
How to calculate Pitching moment?
With Pitching Moment Coefficient (Cm), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁) we can find Pitching moment using the formula - Pitching Moment = Pitching Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length.
Can the Pitching moment be negative?
Yes, the Pitching moment, measured in Moment of Force can be negative.
Which unit is used to measure Pitching moment?
Pitching moment is usually measured using the Newton Meter[N*m] for Moment of Force. Kilonewton Meter[N*m], Millinewton Meter[N*m], Micronewton Meter[N*m] are the few other units in which Pitching moment can be measured.
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