FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Tail Lift Coefficient for given Tail Volume Ratio Formula

Fx Copy

LaTeX Copy

Tail Lift Coefficient is the lift coefficient associated with the tail (only) of an aircraft. It is a dimensionless quantity. Check FAQs

CT lift = - (\frac{Cm t}{V H \cdot η})

CT_lift - Tail Lift Coefficient?Cm_t - Tail Pitching Moment Coefficient?V_H - Horizontal Tail Volume Ratio?η - Tail Efficiency?

Tail Lift Coefficient for given Tail Volume Ratio Example

With values

With units

Only example

Here is how the Tail Lift Coefficient for given Tail Volume Ratio equation looks like with Values.

Here is how the Tail Lift Coefficient for given Tail Volume Ratio equation looks like with Units.

Here is how the Tail Lift Coefficient for given Tail Volume Ratio equation looks like.

0.2985 = - (\frac{-0.39}{1.42 \cdot 0.92})

0.2985 = - (\frac{-0.39}{1.42 \cdot 0.92})

0.2985 = - (\frac{-0.39}{1.42 \cdot 0.92})

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aircraft Mechanics » fx Tail Lift Coefficient for given Tail Volume Ratio

Tail Lift Coefficient for given Tail Volume Ratio Solution

Follow our step by step solution on how to calculate Tail Lift Coefficient for given Tail Volume Ratio?

FIRST Step Consider the formula

CT lift = - (\frac{Cm t}{V H \cdot η})

Next Step Substitute values of Variables

∴

CT lift = - (\frac{-0.39}{1.42 \cdot 0.92})

Next Step Prepare to Evaluate

∴

CT lift = - (\frac{-0.39}{1.42 \cdot 0.92})

Next Step Evaluate

∴

CT lift = 0.298530312308634

LAST Step Rounding Answer

∴

CT lift = 0.2985

Tail Lift Coefficient for given Tail Volume Ratio Formula Elements

Variables

Tail Lift Coefficient

Tail Lift Coefficient is the lift coefficient associated with the tail (only) of an aircraft. It is a dimensionless quantity.

Symbol: CT_lift

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Tail Lift Coefficient

Tail Pitching Moment Coefficient

Tail Pitching Moment Coefficient is the coefficient of pitching moment associated with the horizontal tail of an aircraft.

Symbol: Cm_t

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Tail Pitching Moment Coefficient

Horizontal Tail Volume Ratio

Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft's c.g., the wing area, and the mean aerodynamic wing chord.

Symbol: V_H

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Horizontal Tail Volume Ratio

Tail Efficiency

Tail Efficiency is defined as the ratio of dynamic pressure associated with the tail to dynamic pressure associated with an aircraft's wing.

Symbol: η

Measurement: NAUnit: Unitless

Note: Value should be between 0.8 to 1.2.

Formulas to find Tail Efficiency

Other formulas in Tail Contribution category

Go Tail Pitching Moment for given Lift Coefficient

M t = - \frac{𝒍 t \cdot CT lift \cdot ρ ∞ \cdot {V tail}^{2} \cdot S t}{2}

Go Tail Lift for given Tail Pitching Moment

L t = - (\frac{M t}{𝒍 t})

Go Pitching Moment due to Tail

M t = - 𝒍 t \cdot L t

Go Tail Pitching Moment for given Moment Coefficient

M t = \frac{Cm t \cdot ρ ∞ \cdot V^{2} \cdot S \cdot c ma}{2}

How to Evaluate Tail Lift Coefficient for given Tail Volume Ratio?

Tail Lift Coefficient for given Tail Volume Ratio evaluator uses Tail Lift Coefficient = -(Tail Pitching Moment Coefficient/(Horizontal Tail Volume Ratio*Tail Efficiency)) to evaluate the Tail Lift Coefficient, Tail lift coefficient for given tail volume ratio is a measure of the lift generated by the tail of an aircraft per unit tail volume, taking into account the pitching moment coefficient, tail volume ratio, and tail efficiency, providing a crucial parameter for aircraft design and stability analysis. Tail Lift Coefficient is denoted by CT_lift symbol.

How to evaluate Tail Lift Coefficient for given Tail Volume Ratio using this online evaluator? To use this online evaluator for Tail Lift Coefficient for given Tail Volume Ratio, enter Tail Pitching Moment Coefficient (Cm_t), Horizontal Tail Volume Ratio (V_H) & Tail Efficiency (η) and hit the calculate button.

FAQs on Tail Lift Coefficient for given Tail Volume Ratio

What is the formula to find Tail Lift Coefficient for given Tail Volume Ratio?

The formula of Tail Lift Coefficient for given Tail Volume Ratio is expressed as Tail Lift Coefficient = -(Tail Pitching Moment Coefficient/(Horizontal Tail Volume Ratio*Tail Efficiency)). Here is an example- 0.3 = -((-0.39)/(1.42*0.92)).

How to calculate Tail Lift Coefficient for given Tail Volume Ratio?

With Tail Pitching Moment Coefficient (Cm_t), Horizontal Tail Volume Ratio (V_H) & Tail Efficiency (η) we can find Tail Lift Coefficient for given Tail Volume Ratio using the formula - Tail Lift Coefficient = -(Tail Pitching Moment Coefficient/(Horizontal Tail Volume Ratio*Tail Efficiency)).

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Tail Lift Coefficient for given Tail Volume Ratio Formula

Tail Lift Coefficient for given Tail Volume Ratio Example

Tail Lift Coefficient for given Tail Volume Ratio Solution

Tail Lift Coefficient for given Tail Volume Ratio Formula Elements

Other formulas in Tail Contribution category

How to Evaluate Tail Lift Coefficient for given Tail Volume Ratio?

FAQs on Tail Lift Coefficient for given Tail Volume Ratio

Variable Name