Yawing Moment Calculator

✖Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis.ⓘ Yawing Moment Coefficient [C_n]			+10% -10%
✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic Pressure [q]			+10% -10%
✖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.ⓘ Reference Area [S]			+10% -10%
✖Characteristic Length (used in aerodynamics) is a reference length characteristic of the object under consideration.ⓘ Characteristic Length [𝓁]			+10% -10%

✖Yawing Moment is the moment acting on the airplane about its yaw axis.ⓘ Yawing Moment [𝑵]

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Yawing Moment Solution

STEP 0: Pre-Calculation Summary

Formula Used

Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length
𝑵 = C_n*q*S*𝓁
This formula uses 5 Variables

Variables Used

Yawing Moment - (Measured in Newton Meter) - Yawing Moment is the moment acting on the airplane about its yaw axis.
Yawing Moment Coefficient - Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis.
Dynamic Pressure - (Measured in Pascal) - Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Reference Area - (Measured in Square Meter) - 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.
Characteristic Length - (Measured in Meter) - Characteristic Length (used in aerodynamics) is a reference length characteristic of the object under consideration.

STEP 1: Convert Input(s) to Base Unit

Yawing Moment Coefficient: 1.4 --> No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
Reference Area: 5.08 Square Meter --> 5.08 Square Meter No Conversion Required
Characteristic Length: 0.6 Meter --> 0.6 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

𝑵 = C_n*q*S*𝓁 --> 1.4*10*5.08*0.6

Evaluating ... ...

𝑵 = 42.672

STEP 3: Convert Result to Output's Unit

42.672 Newton Meter --> No Conversion Required

FINAL ANSWER

42.672 Newton Meter <-- Yawing Moment

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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< Aircraft Dynamics Nomenclature Calculators

Aerodynamic Normal Force

LaTeX Go Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area

Aerodynamic Axial Force

LaTeX Go Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area

Side force coefficient

LaTeX Go Side Force Coefficient = Aerodynamic Side Force/(Dynamic Pressure*Reference Area)

Aerodynamic Side Force

LaTeX Go Aerodynamic Side Force = Side Force Coefficient*Dynamic Pressure*Reference Area

Yawing Moment Formula

LaTeX Go

Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length
𝑵 = C_n*q*S*𝓁

What is the characteristic length for calculating yawing moment?

Characteristic length is taken as the wing span for the yawing moment of an aircraft. The wingspan of an aircraft is always measured in a straight line, from wingtip to wingtip, independently of wing shape or sweep.

How to Calculate Yawing Moment?

Yawing Moment calculator uses Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length to calculate the Yawing Moment, Yawing Moment is a measure of the rotational force that causes an aircraft to turn or yaw around its vertical axis, affected by factors such as air density, wing surface area, and length of the aircraft, it is a critical parameter in aerodynamics, influencing the stability and control of an aircraft during flight. Yawing Moment is denoted by 𝑵 symbol.

How to calculate Yawing Moment using this online calculator? To use this online calculator for Yawing Moment, enter Yawing Moment Coefficient (C_n), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁) and hit the calculate button. Here is how the Yawing Moment calculation can be explained with given input values -> 42.672 = 1.4*10*5.08*0.6.

FAQ

What is Yawing Moment?

Yawing Moment is a measure of the rotational force that causes an aircraft to turn or yaw around its vertical axis, affected by factors such as air density, wing surface area, and length of the aircraft, it is a critical parameter in aerodynamics, influencing the stability and control of an aircraft during flight and is represented as 𝑵 = C_n*q*S*𝓁 or Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length. Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis, Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid, 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 & Characteristic Length (used in aerodynamics) is a reference length characteristic of the object under consideration.

How to calculate Yawing Moment?

Yawing Moment is a measure of the rotational force that causes an aircraft to turn or yaw around its vertical axis, affected by factors such as air density, wing surface area, and length of the aircraft, it is a critical parameter in aerodynamics, influencing the stability and control of an aircraft during flight is calculated using Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length. To calculate Yawing Moment, you need Yawing Moment Coefficient (C_n), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁). With our tool, you need to enter the respective value for Yawing Moment Coefficient, Dynamic Pressure, Reference Area & Characteristic Length and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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