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Minimum Flight Velocity Formula

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Minimum Flight Velocity is the velocity of the aircraft such that air passes over the wings fast enough for the aircraft to sustain constant altitude. Check FAQs

V min = \sqrt{(\frac{W}{5}) \cdot (\frac{2}{ρ}) \cdot (\frac{1}{C L})}

V_min - Minimum Flight Velocity?W - Aircraft Weight?5 - Aircraft Gross Wing Area?ρ - Air Density?C_L - Lift Coefficient?

Minimum Flight Velocity Example

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Here is how the Minimum Flight Velocity equation looks like with Values.

Here is how the Minimum Flight Velocity equation looks like with Units.

Here is how the Minimum Flight Velocity equation looks like.

589.9388 = \sqrt{(\frac{1800}{4}) \cdot (\frac{2}{1.293}) \cdot (\frac{1}{0.002})}

589.9388m/s = \sqrt{(\frac{1800N}{4m²}) \cdot (\frac{2}{1.293kg/m³}) \cdot (\frac{1}{0.002})}

589.9388 = \sqrt{(\frac{1800}{4}) \cdot (\frac{2}{1.293}) \cdot (\frac{1}{0.002})}

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Minimum Flight Velocity Solution

Follow our step by step solution on how to calculate Minimum Flight Velocity?

FIRST Step Consider the formula

V min = \sqrt{(\frac{W}{5}) \cdot (\frac{2}{ρ}) \cdot (\frac{1}{C L})}

Next Step Substitute values of Variables

∴

V min = \sqrt{(\frac{1800N}{4m²}) \cdot (\frac{2}{1.293kg/m³}) \cdot (\frac{1}{0.002})}

Next Step Prepare to Evaluate

∴

V min = \sqrt{(\frac{1800}{4}) \cdot (\frac{2}{1.293}) \cdot (\frac{1}{0.002})}

Next Step Evaluate

∴

V min = 589.938846175922m/s

LAST Step Rounding Answer

∴

V min = 589.9388m/s

Minimum Flight Velocity Formula Elements

Variables

Functions

Minimum Flight Velocity

Minimum Flight Velocity is the velocity of the aircraft such that air passes over the wings fast enough for the aircraft to sustain constant altitude.

Symbol: V_min

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Minimum Flight Velocity

Aircraft Weight

Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.

Symbol: W

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Aircraft Weight

Aircraft Gross Wing Area

Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.

Symbol: 5

Measurement: AreaUnit: m²

Note: Value can be positive or negative.

Formulas to find Aircraft Gross Wing Area

Air Density

Air Density denoted ρ, is the mass per unit volume of Earth's atmosphere.

Symbol: ρ

Measurement: DensityUnit: kg/m³

Note: Value should be greater than 0.

Formulas to find Air Density

Lift Coefficient

The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

Symbol: C_L

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient

sqrt

A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.

Syntax: sqrt(Number)

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How to Evaluate Minimum Flight Velocity?

Minimum Flight Velocity evaluator uses Minimum Flight Velocity = sqrt((Aircraft Weight/Aircraft Gross Wing Area)*(2/(Air Density))*(1/Lift Coefficient)) to evaluate the Minimum Flight Velocity, Minimum Flight Velocity of an aircraft, often referred to as the stall speed, is the lowest speed at which the aircraft can maintain controlled flight without stalling, stalling occurs when the airflow over the wings becomes too disrupted, leading to a loss of lift. Minimum Flight Velocity is denoted by V_min symbol.

How to evaluate Minimum Flight Velocity using this online evaluator? To use this online evaluator for Minimum Flight Velocity, enter Aircraft Weight (W), Aircraft Gross Wing Area (5), Air Density (ρ) & Lift Coefficient (C_L) and hit the calculate button.

FAQs on Minimum Flight Velocity

What is the formula to find Minimum Flight Velocity?

The formula of Minimum Flight Velocity is expressed as Minimum Flight Velocity = sqrt((Aircraft Weight/Aircraft Gross Wing Area)*(2/(Air Density))*(1/Lift Coefficient)). Here is an example- 589.9388 = sqrt((1800/4)*(2/(1.293))*(1/0.002)).

How to calculate Minimum Flight Velocity?

With Aircraft Weight (W), Aircraft Gross Wing Area (5), Air Density (ρ) & Lift Coefficient (C_L) we can find Minimum Flight Velocity using the formula - Minimum Flight Velocity = sqrt((Aircraft Weight/Aircraft Gross Wing Area)*(2/(Air Density))*(1/Lift Coefficient)). This formula also uses Square Root Function function(s).

Can the Minimum Flight Velocity be negative?

No, the Minimum Flight Velocity, measured in Speed cannot be negative.

Which unit is used to measure Minimum Flight Velocity?

Minimum Flight 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 Minimum Flight Velocity can be measured.

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Minimum Flight Velocity Formula

Minimum Flight Velocity Example

Minimum Flight Velocity Solution

Minimum Flight Velocity Formula Elements

Other formulas in High Load Factor Maneuver category

How to Evaluate Minimum Flight Velocity?

FAQs on Minimum Flight Velocity

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