Flight Speed given Dynamic Pressure Formula

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Flight Speed is defined as an airspeed sufficient to provide the lift necessary to support an airplane in level flight. Check FAQs
Vfs=2qρ
Vfs - Flight Speed?q - Dynamic Pressure?ρ - Ambient Air Density?

Flight Speed given Dynamic Pressure Example

With values
With units
Only example

Here is how the Flight Speed given Dynamic Pressure equation looks like with Values.

Here is how the Flight Speed given Dynamic Pressure equation looks like with Units.

Here is how the Flight Speed given Dynamic Pressure equation looks like.

10.7286Edit=270.5Edit1.225Edit
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Flight Speed given Dynamic Pressure Solution

Follow our step by step solution on how to calculate Flight Speed given Dynamic Pressure?

FIRST Step Consider the formula
Vfs=2qρ
Next Step Substitute values of Variables
Vfs=270.5Pa1.225kg/m³
Next Step Prepare to Evaluate
Vfs=270.51.225
Next Step Evaluate
Vfs=10.7285619174392m/s
LAST Step Rounding Answer
Vfs=10.7286m/s

Flight Speed given Dynamic Pressure Formula Elements

Variables
Functions
Flight Speed
Flight Speed is defined as an airspeed sufficient to provide the lift necessary to support an airplane in level flight.
Symbol: Vfs
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Dynamic Pressure
Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Symbol: q
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
Ambient Air Density
Ambient Air Density is the mass per unit volume of Earth's atmosphere.
Symbol: ρ
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
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 Preliminary Aerodynamics category

​Go Velocity at Sea-Level given Lift Coefficient
V0=2Wbody[Std-Air-Density-Sea]SCL
​Go Power required at sea-level conditions
PR,0=2Wbody3CD2[Std-Air-Density-Sea]SCL3
​Go Velocity at Altitude
Valt=2Wbodyρ0SCL
​Go Power required at Altitude
PR,alt=2Wbody3CD2ρ0SCL3

How to Evaluate Flight Speed given Dynamic Pressure?

Flight Speed given Dynamic Pressure evaluator uses Flight Speed = sqrt((2*Dynamic Pressure)/Ambient Air Density) to evaluate the Flight Speed, Flight Speed given Dynamic Pressure is a measure of the speed of an object, such as an aircraft, calculated based on the dynamic pressure and ambient air density, it is a fundamental concept in aerodynamics, where the dynamic pressure is a measure of the air pressure exerted on an object moving through the air, and the ambient air density is the density of the air surrounding the object. Flight Speed is denoted by Vfs symbol.

How to evaluate Flight Speed given Dynamic Pressure using this online evaluator? To use this online evaluator for Flight Speed given Dynamic Pressure, enter Dynamic Pressure (q) & Ambient Air Density (ρ) and hit the calculate button.

FAQs on Flight Speed given Dynamic Pressure

What is the formula to find Flight Speed given Dynamic Pressure?
The formula of Flight Speed given Dynamic Pressure is expressed as Flight Speed = sqrt((2*Dynamic Pressure)/Ambient Air Density). Here is an example- 10.72856 = sqrt((2*70.5)/1.225).
How to calculate Flight Speed given Dynamic Pressure?
With Dynamic Pressure (q) & Ambient Air Density (ρ) we can find Flight Speed given Dynamic Pressure using the formula - Flight Speed = sqrt((2*Dynamic Pressure)/Ambient Air Density). This formula also uses Square Root (sqrt) function(s).
Can the Flight Speed given Dynamic Pressure be negative?
No, the Flight Speed given Dynamic Pressure, measured in Speed cannot be negative.
Which unit is used to measure Flight Speed given Dynamic Pressure?
Flight Speed given Dynamic Pressure 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 Flight Speed given Dynamic Pressure can be measured.
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