FormulaDen.com

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

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Formula

Fx Copy

LaTeX Copy

Vehicle Speed (True Air Speed) of an aircraft is the speed of aircraft relative to air mass through which it is flying. The true airspeed is important information for accurate navigation of aircraft. Check FAQs

V = \sqrt{\frac{2 \cdot M Aircraft \cdot [g]}{ρ \cdot S \cdot C L,max}}

V - Vehicle Speed?M_Aircraft - Mass Aircraft?ρ - Density Altitude for flying?S - Aircraft Gross Wing Area?C_L,max - Maximum Lift Coefficient?[g] - Gravitational acceleration on Earth?

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Example

With values

With units

Only example

Here is how the Vehicle Stalling Speed given Maximum Attainable Lift Coefficient equation looks like with Values.

Here is how the Vehicle Stalling Speed given Maximum Attainable Lift Coefficient equation looks like with Units.

Here is how the Vehicle Stalling Speed given Maximum Attainable Lift Coefficient equation looks like.

200.1071 = \sqrt{\frac{2 \cdot 50000 \cdot 9.8066}{1.21 \cdot 23 \cdot 0.88}}

200.1071km/h = \sqrt{\frac{2 \cdot 50000kg \cdot 9.8066m/s²}{1.21kg/m³ \cdot 23m² \cdot 0.88}}

200.1071 = \sqrt{\frac{2 \cdot 50000 \cdot 9.8066}{1.21 \cdot 23 \cdot 0.88}}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Engineering » Category

Civil » Category

Transportation Engineering » fx Vehicle Stalling Speed given Maximum Attainable Lift Coefficient

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Solution

Follow our step by step solution on how to calculate Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

FIRST Step Consider the formula

V = \sqrt{\frac{2 \cdot M Aircraft \cdot [g]}{ρ \cdot S \cdot C L,max}}

Next Step Substitute values of Variables

∴

V = \sqrt{\frac{2 \cdot 50000kg \cdot [g]}{1.21kg/m³ \cdot 23m² \cdot 0.88}}

Next Step Substitute values of Constants

∴

V = \sqrt{\frac{2 \cdot 50000kg \cdot 9.8066m/s²}{1.21kg/m³ \cdot 23m² \cdot 0.88}}

Next Step Prepare to Evaluate

∴

V = \sqrt{\frac{2 \cdot 50000 \cdot 9.8066}{1.21 \cdot 23 \cdot 0.88}}

Next Step Evaluate

∴

V = 55.5852928121744m/s

Next Step Convert to Output's Unit

∴

V = 200.107054123828km/h

LAST Step Rounding Answer

∴

V = 200.1071km/h

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Formula Elements

Variables

Constants

Functions

Vehicle Speed

Vehicle Speed (True Air Speed) of an aircraft is the speed of aircraft relative to air mass through which it is flying. The true airspeed is important information for accurate navigation of aircraft.

Symbol: V

Measurement: SpeedUnit: km/h

Note: Value can be positive or negative.

Formulas to find Vehicle Speed

Mass Aircraft

Mass Aircraft is the quantity of matter in a body regardless of its volume or of any forces acting on it.

Symbol: M_Aircraft

Measurement: WeightUnit: kg

Note: Value can be positive or negative.

Formulas to find Mass Aircraft

Density Altitude for flying

Density Altitude for flying is a representation of the amount of mass of a substance, material or object in relation to the space it occupies at an altitude.

Symbol: ρ

Measurement: DensityUnit: kg/m³

Note: Value can be positive or negative.

Formulas to find Density Altitude for flying

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: S

Measurement: AreaUnit: m²

Note: Value can be positive or negative.

Formulas to find Aircraft Gross Wing Area

Maximum Lift Coefficient

Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.

Symbol: C_L,max

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Maximum Lift Coefficient

Gravitational acceleration on Earth

Gravitational acceleration on Earth means that the velocity of an object in free fall will increase by 9.8 m/s2 every second.

Symbol: [g]

Value: 9.80665 m/s²

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)

Other formulas in Aircraft Gross Wing category

Go Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle

S = \frac{L Aircraft}{0.5 \cdot ρ \cdot V^{2} \cdot C l}

Go Aircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions

S = 2 \cdot M Aircraft \cdot \frac{[g]}{ρ \cdot C l \cdot V^{2}}

Go Maximum Attainable Lift Coefficient given Vehicle Stalling Speed

C L,max = 2 \cdot M Aircraft \cdot \frac{[g]}{ρ \cdot S \cdot V^{2}}

Go Aircraft Gross Wing Area given Vehicle Stalling Speed

S = 2 \cdot M Aircraft \cdot \frac{[g]}{V^{2} \cdot ρ \cdot C L,max}

How to Evaluate Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient evaluator uses Vehicle Speed = sqrt((2*Mass Aircraft*[g])/(Density Altitude for flying*Aircraft Gross Wing Area*Maximum Lift Coefficient)) to evaluate the Vehicle Speed, Vehicle Stalling Speed given Maximum Attainable Lift Coefficient is defined as is minimum speed at which aircraft must fly in order to stay aloft. Vehicle Speed is denoted by V symbol.

How to evaluate Vehicle Stalling Speed given Maximum Attainable Lift Coefficient using this online evaluator? To use this online evaluator for Vehicle Stalling Speed given Maximum Attainable Lift Coefficient, enter Mass Aircraft (M_Aircraft), Density Altitude for flying (ρ), Aircraft Gross Wing Area (S) & Maximum Lift Coefficient (C_L,max) and hit the calculate button.

FAQs on Vehicle Stalling Speed given Maximum Attainable Lift Coefficient

What is the formula to find Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

The formula of Vehicle Stalling Speed given Maximum Attainable Lift Coefficient is expressed as Vehicle Speed = sqrt((2*Mass Aircraft*[g])/(Density Altitude for flying*Aircraft Gross Wing Area*Maximum Lift Coefficient)). Here is an example- 720.3854 = sqrt((2*50000*[g])/(1.21*23*0.88)).

How to calculate Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

With Mass Aircraft (M_Aircraft), Density Altitude for flying (ρ), Aircraft Gross Wing Area (S) & Maximum Lift Coefficient (C_L,max) we can find Vehicle Stalling Speed given Maximum Attainable Lift Coefficient using the formula - Vehicle Speed = sqrt((2*Mass Aircraft*[g])/(Density Altitude for flying*Aircraft Gross Wing Area*Maximum Lift Coefficient)). This formula also uses Gravitational acceleration on Earth constant(s) and Square Root (sqrt) function(s).

Can the Vehicle Stalling Speed given Maximum Attainable Lift Coefficient be negative?

Yes, the Vehicle Stalling Speed given Maximum Attainable Lift Coefficient, measured in Speed can be negative.

Which unit is used to measure Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient is usually measured using the Kilometer per Hour[km/h] for Speed. Meter per Second[km/h], Meter per Minute[km/h], Meter per Hour[km/h] are the few other units in which Vehicle Stalling Speed given Maximum Attainable Lift Coefficient can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Formula

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Example

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Solution

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient Formula Elements

Other formulas in Aircraft Gross Wing category

How to Evaluate Vehicle Stalling Speed given Maximum Attainable Lift Coefficient?

FAQs on Vehicle Stalling Speed given Maximum Attainable Lift Coefficient

Variable Name