Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency 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%
✖Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft's e.g., the wing area, and the wingspan.ⓘ Vertical Tail Volume Ratio [V_v]			+10% -10%
✖Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.ⓘ Vertical Tail Efficiency [η_v]			+10% -10%
✖The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft.ⓘ Vertical Tail Lift Curve Slope [C_v]			+10% -10%
✖Sidewash Angle is caused by the flow field distortion due to the wings and fuselage. It is analogous to the downwash angle for the horizontal tailplane.ⓘ Sidewash Angle [σ]			+10% -10%

✖The Sideslip Angle, also called the angle of sideslip, is a term used in fluid dynamics and aerodynamics, and aviation which relates to the rotation of the aircraft centerline from the relative wind.ⓘ Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency [β]

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Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency Solution

STEP 0: Pre-Calculation Summary

Formula Used

Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Volume Ratio*Vertical Tail Efficiency*Vertical Tail Lift Curve Slope))-Sidewash Angle
β = (C_n/(V_v*η_v*C_v))-σ
This formula uses 6 Variables

Variables Used

Sideslip Angle - (Measured in Radian) - The Sideslip Angle, also called the angle of sideslip, is a term used in fluid dynamics and aerodynamics, and aviation which relates to the rotation of the aircraft centerline from the relative wind.
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.
Vertical Tail Volume Ratio - Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft's e.g., the wing area, and the wingspan.
Vertical Tail Efficiency - Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.
Vertical Tail Lift Curve Slope - (Measured in 1 per Radian) - The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft.
Sidewash Angle - (Measured in Radian) - Sidewash Angle is caused by the flow field distortion due to the wings and fuselage. It is analogous to the downwash angle for the horizontal tailplane.

STEP 1: Convert Input(s) to Base Unit

Yawing Moment Coefficient: 1.4 --> No Conversion Required
Vertical Tail Volume Ratio: 1.02 --> No Conversion Required
Vertical Tail Efficiency: 16.66 --> No Conversion Required
Vertical Tail Lift Curve Slope: 0.7 1 per Radian --> 0.7 1 per Radian No Conversion Required
Sidewash Angle: 0.067 Radian --> 0.067 Radian No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

β = (C_n/(V_v*η_v*C_v))-σ --> (1.4/(1.02*16.66*0.7))-0.067

Evaluating ... ...

β = 0.0506941364781206

STEP 3: Convert Result to Output's Unit

0.0506941364781206 Radian --> No Conversion Required

FINAL ANSWER

0.0506941364781206 ≈ 0.050694 Radian <-- Sideslip Angle

(Calculation completed in 00.006 seconds)

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Created by Vinay Mishra

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

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< Aerodynamic Parameters Calculators

Sidewash Angle for given Moment Produced by Vertical Tail

LaTeX Go Sidewash Angle = (Vertical Tail Moment/(Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*Vertical Tail Dynamic Pressure*Vertical Tail Area))-Sideslip Angle

Yawing Moment Coefficient using Wingspan

LaTeX Go Yawing Moment Coefficient = Vertical Tail Moment/(Wing Dynamic Pressure*Reference Area*Wingspan)

Sideslip Angle for Aircraft

LaTeX Go Sideslip Angle = Vertical Tail Angle of Attack-Sidewash Angle

Sidewash angle

LaTeX Go Sidewash Angle = Vertical Tail Angle of Attack-Sideslip Angle

Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency Formula

LaTeX Go

Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Volume Ratio*Vertical Tail Efficiency*Vertical Tail Lift Curve Slope))-Sidewash Angle
β = (C_n/(V_v*η_v*C_v))-σ

What is aircraft sideslip?

Intentional slip, either forward slip or sideslip, is an intentional cross control maneuver in which the pilot makes an aileron input in one direction with a simultaneous rudder input in the opposite direction.

How to Calculate Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency?

Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency calculator uses Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Volume Ratio*Vertical Tail Efficiency*Vertical Tail Lift Curve Slope))-Sidewash Angle to calculate the Sideslip Angle, Sideslip angle given yawing moment coefficient and tail efficiency describes the relationship between an aircraft's sideslip angle and its yawing moment coefficient, taking into account the vertical tail volume ratio, efficiency, and lift curve slope, as well as the sidewash angle, providing valuable insights for aerodynamic analysis and aircraft design. Sideslip Angle is denoted by β symbol.

How to calculate Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency using this online calculator? To use this online calculator for Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency, enter Yawing Moment Coefficient (C_n), Vertical Tail Volume Ratio (V_v), Vertical Tail Efficiency (η_v), Vertical Tail Lift Curve Slope (C_v) & Sidewash Angle (σ) and hit the calculate button. Here is how the Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency calculation can be explained with given input values -> 0.050694 = (1.4/(1.02*16.66*0.7))-0.067.

FAQ

What is Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency?

Sideslip angle given yawing moment coefficient and tail efficiency describes the relationship between an aircraft's sideslip angle and its yawing moment coefficient, taking into account the vertical tail volume ratio, efficiency, and lift curve slope, as well as the sidewash angle, providing valuable insights for aerodynamic analysis and aircraft design and is represented as β = (C_n/(V_v*η_v*C_v))-σ or Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Volume Ratio*Vertical Tail Efficiency*Vertical Tail Lift Curve Slope))-Sidewash Angle. Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis, Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft's e.g., the wing area, and the wingspan, Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft, The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft & Sidewash Angle is caused by the flow field distortion due to the wings and fuselage. It is analogous to the downwash angle for the horizontal tailplane.

How to calculate Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency?

Sideslip angle given yawing moment coefficient and tail efficiency describes the relationship between an aircraft's sideslip angle and its yawing moment coefficient, taking into account the vertical tail volume ratio, efficiency, and lift curve slope, as well as the sidewash angle, providing valuable insights for aerodynamic analysis and aircraft design is calculated using Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Volume Ratio*Vertical Tail Efficiency*Vertical Tail Lift Curve Slope))-Sidewash Angle. To calculate Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency, you need Yawing Moment Coefficient (C_n), Vertical Tail Volume Ratio (V_v), Vertical Tail Efficiency (η_v), Vertical Tail Lift Curve Slope (C_v) & Sidewash Angle (σ). With our tool, you need to enter the respective value for Yawing Moment Coefficient, Vertical Tail Volume Ratio, Vertical Tail Efficiency, Vertical Tail Lift Curve Slope & Sidewash Angle and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Sideslip Angle?

In this formula, Sideslip Angle uses Yawing Moment Coefficient, Vertical Tail Volume Ratio, Vertical Tail Efficiency, Vertical Tail Lift Curve Slope & Sidewash Angle. We can use 3 other way(s) to calculate the same, which is/are as follows -

Sideslip Angle = Vertical Tail Angle of Attack-Sidewash Angle
Sideslip Angle = (Vertical Tail Moment/(Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*Vertical Tail Dynamic Pressure*Vertical Tail Area))-Sidewash Angle
Sideslip Angle = (Yawing Moment Coefficient/(Vertical Tail Moment Arm*Vertical Tail Area*Vertical Tail Dynamic Pressure*Vertical Tail Lift Curve Slope/(Reference Area*Wingspan*Wing Dynamic Pressure)))-Sidewash Angle

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