Rolling Moment Formula

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Rolling Moment is the moment acting on the airplane about its roll axis. Check FAQs
𝑳=C𝒍qS𝓁
𝑳 - Rolling Moment?C𝒍 - Rolling Moment Coefficient?q - Dynamic Pressure?S - Reference Area?𝓁 - Characteristic Length?

Rolling Moment Example

With values
With units
Only example

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

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

Here is how the Rolling Moment equation looks like.

18.5928Edit=0.61Edit10Edit5.08Edit0.6Edit
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Rolling Moment Solution

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

FIRST Step Consider the formula
𝑳=C𝒍qS𝓁
Next Step Substitute values of Variables
𝑳=0.6110Pa5.080.6m
Next Step Prepare to Evaluate
𝑳=0.61105.080.6
LAST Step Evaluate
𝑳=18.5928N*m

Rolling Moment Formula Elements

Variables
Rolling Moment
Rolling Moment is the moment acting on the airplane about its roll axis.
Symbol: 𝑳
Measurement: Moment of ForceUnit: N*m
Note: Value can be positive or negative.
Rolling Moment Coefficient
Rolling Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its roll axis.
Symbol: C𝒍
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 Rolling Moment?

Rolling Moment evaluator uses Rolling Moment = Rolling Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length to evaluate the Rolling Moment, The Rolling Moment is a measure of the turning force that causes an object to rotate around a pivot point, resulting from the interaction between the object and a fluid, such as air or water, and is a critical concept in aerodynamics, hydrodynamics, and engineering, it is used to analyze and predict the behavior of aircraft, ships, and other objects in motion. Rolling Moment is denoted by 𝑳 symbol.

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

FAQs on Rolling Moment

What is the formula to find Rolling Moment?
The formula of Rolling Moment is expressed as Rolling Moment = Rolling Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length. Here is an example- 18.5928 = 0.61*10*5.08*0.6.
How to calculate Rolling Moment?
With Rolling Moment Coefficient (C𝒍), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁) we can find Rolling Moment using the formula - Rolling Moment = Rolling Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length.
Can the Rolling Moment be negative?
Yes, the Rolling Moment, measured in Moment of Force can be negative.
Which unit is used to measure Rolling Moment?
Rolling 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 Rolling Moment can be measured.
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