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Stall velocity for given liftoff velocity Formula

GoStall velocity for given weight Formula

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Stall Velocity is defined as the velocity of an airplane in steady flight at its maximum lift coefficient. Check FAQs

V stall = \frac{V LO}{1.2}

V_stall - Stall Velocity?V_LO - Liftoff velocity?

Stall velocity for given liftoff velocity Example

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Here is how the Stall velocity for given liftoff velocity equation looks like with Values.

Here is how the Stall velocity for given liftoff velocity equation looks like with Units.

Here is how the Stall velocity for given liftoff velocity equation looks like.

148 = \frac{177.6}{1.2}

148m/s = \frac{177.6m/s}{1.2}

148 = \frac{177.6}{1.2}

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Stall velocity for given liftoff velocity Solution

Follow our step by step solution on how to calculate Stall velocity for given liftoff velocity?

FIRST Step Consider the formula

V stall = \frac{V LO}{1.2}

Next Step Substitute values of Variables

∴

V stall = \frac{177.6m/s}{1.2}

Next Step Prepare to Evaluate

∴

V stall = \frac{177.6}{1.2}

LAST Step Evaluate

∴

V stall = 148m/s

Stall velocity for given liftoff velocity Formula Elements

Variables

Stall Velocity

Stall Velocity is defined as the velocity of an airplane in steady flight at its maximum lift coefficient.

Symbol: V_stall

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Stall Velocity

Liftoff velocity

Liftoff velocity is defined as the velocity of the aircraft at which it first becomes airborne.

Symbol: V_LO

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Liftoff velocity

Other Formulas to find Stall Velocity

Go Stall velocity for given weight

V stall = \sqrt{\frac{2 \cdot W}{ρ ∞ \cdot S \cdot C L,max}}

Other formulas in Take Off category

Go Resistance force during ground roll

R = μ r \cdot (W - F L)

Go Coefficient of rolling friction during ground roll

μ r = \frac{R}{W - F L}

Go Weight of aircraft during ground roll

W = (\frac{R}{μ r}) + F L

Go Lift acting on aircraft during ground roll

F L = W - (\frac{R}{μ r})

How to Evaluate Stall velocity for given liftoff velocity?

Stall velocity for given liftoff velocity evaluator uses Stall Velocity = Liftoff velocity/1.2 to evaluate the Stall Velocity, Stall Velocity for Given Liftoff Velocity is the minimum speed at which an aircraft can maintain level flight, calculated by dividing the liftoff velocity by 1.2. Stall Velocity is denoted by V_stall symbol.

How to evaluate Stall velocity for given liftoff velocity using this online evaluator? To use this online evaluator for Stall velocity for given liftoff velocity, enter Liftoff velocity (V_LO) and hit the calculate button.

FAQs on Stall velocity for given liftoff velocity

What is the formula to find Stall velocity for given liftoff velocity?

The formula of Stall velocity for given liftoff velocity is expressed as Stall Velocity = Liftoff velocity/1.2. Here is an example- 77.5 = 177.6/1.2.

How to calculate Stall velocity for given liftoff velocity?

With Liftoff velocity (V_LO) we can find Stall velocity for given liftoff velocity using the formula - Stall Velocity = Liftoff velocity/1.2.

What are the other ways to Calculate Stall Velocity?

Here are the different ways to Calculate Stall Velocity-

Stall Velocity=sqrt((2*Weight)/(Freestream Density*Reference Area*Maximum Lift Coefficient))

Can the Stall velocity for given liftoff velocity be negative?

No, the Stall velocity for given liftoff velocity, measured in Speed cannot be negative.

Which unit is used to measure Stall velocity for given liftoff velocity?

Stall velocity for given liftoff velocity is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Stall velocity for given liftoff velocity can be measured.

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