FormulaDen.com

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

Average Blade Lift Coefficient Formula

Fx Copy

LaTeX Copy

Blade Lift Coefficient is the lift coefficient of blades and is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body. Check FAQs

C l = 6 \cdot \frac{C T}{σ}

C_l - Blade Lift Coefficient?C_T - Thrust Coefficient?σ - Rotor Solidity?

Average Blade Lift Coefficient Example

With values

With units

Only example

Here is how the Average Blade Lift Coefficient equation looks like with Values.

Here is how the Average Blade Lift Coefficient equation looks like with Units.

Here is how the Average Blade Lift Coefficient equation looks like.

0.4 = 6 \cdot \frac{0.04}{0.6}

0.4 = 6 \cdot \frac{0.04}{0.6}

0.4 = 6 \cdot \frac{0.04}{0.6}

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 Average Blade Lift Coefficient

Average Blade Lift Coefficient Solution

Follow our step by step solution on how to calculate Average Blade Lift Coefficient?

FIRST Step Consider the formula

C l = 6 \cdot \frac{C T}{σ}

Next Step Substitute values of Variables

∴

C l = 6 \cdot \frac{0.04}{0.6}

Next Step Prepare to Evaluate

∴

C l = 6 \cdot \frac{0.04}{0.6}

LAST Step Evaluate

∴

C l = 0.4

Average Blade Lift Coefficient Formula Elements

Variables

Blade Lift Coefficient

Blade Lift Coefficient is the lift coefficient of blades and is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body.

Symbol: C_l

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Blade Lift Coefficient

Thrust Coefficient

Thrust Coefficient is the ratio of actual thrust to the ideal thrust.

Symbol: C_T

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Thrust Coefficient

Rotor Solidity

Rotor Solidity is a function of the aspect ratio and number of blades in the rotor.

Symbol: σ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Rotor Solidity

Other formulas in Structural Design category

Go Maximum Blade Efficiency

n bm = \frac{2 \cdot \frac{F l}{F d} - 1}{2 \cdot \frac{F l}{F d} + 1}

Go Disk Loading

W load = \frac{W a}{\frac{π \cdot {d r}^{2}}{4}}

Go Shear Load per width

P = \frac{π \cdot (D^{2}) \cdot 𝜏 max}{4 \cdot b}

Go Allowable Bearing Pressure

f br = \frac{P \cdot b}{p t \cdot D rivet}

How to Evaluate Average Blade Lift Coefficient?

Average Blade Lift Coefficient evaluator uses Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity to evaluate the Blade Lift Coefficient, The Average Blade Lift Coefficient refers to the average value of the lift coefficient across the entire rotor blade of a helicopter or a similar rotary-wing aircraft, the lift coefficient quantifies the lift generation capability of an airfoil and is a crucial parameter in determining the aircraft's performance characteristics. Blade Lift Coefficient is denoted by C_l symbol.

How to evaluate Average Blade Lift Coefficient using this online evaluator? To use this online evaluator for Average Blade Lift Coefficient, enter Thrust Coefficient (C_T) & Rotor Solidity (σ) and hit the calculate button.

FAQs on Average Blade Lift Coefficient

What is the formula to find Average Blade Lift Coefficient?

The formula of Average Blade Lift Coefficient is expressed as Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity. Here is an example- 4 = 6*0.04/Solodity_of_rotor_helicopter.

How to calculate Average Blade Lift Coefficient?

With Thrust Coefficient (C_T) & Rotor Solidity (σ) we can find Average Blade Lift Coefficient using the formula - Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Average Blade Lift Coefficient Formula

Average Blade Lift Coefficient Example

Average Blade Lift Coefficient Solution

Average Blade Lift Coefficient Formula Elements

Other formulas in Structural Design category

How to Evaluate Average Blade Lift Coefficient?

FAQs on Average Blade Lift Coefficient

Variable Name