Velocity at Sea-Level given Lift Coefficient Formula

Fx Copy
LaTeX Copy
Velocity at Sea-Level is the distance traveled per unit of time by aircraft at sea-level conditions. Check FAQs
V0=2Wbody[Std-Air-Density-Sea]SCL
V0 - Velocity at Sea-Level?Wbody - Weight of Body?S - Reference Area?CL - Lift Coefficient?[Std-Air-Density-Sea] - Standard air density at sea-level conditions?

Velocity at Sea-Level given Lift Coefficient Example

With values
With units
Only example

Here is how the Velocity at Sea-Level given Lift Coefficient equation looks like with Values.

Here is how the Velocity at Sea-Level given Lift Coefficient equation looks like with Units.

Here is how the Velocity at Sea-Level given Lift Coefficient equation looks like.

6.7988Edit=2750Edit1.22991.05Edit0.29Edit
You are here -
HomeIcon Home » Category Physics » Category Aerospace » Category Aircraft Mechanics » fx Velocity at Sea-Level given Lift Coefficient

Velocity at Sea-Level given Lift Coefficient Solution

Follow our step by step solution on how to calculate Velocity at Sea-Level given Lift Coefficient?

FIRST Step Consider the formula
V0=2Wbody[Std-Air-Density-Sea]SCL
Next Step Substitute values of Variables
V0=2750N[Std-Air-Density-Sea]91.050.29
Next Step Substitute values of Constants
V0=2750N1.22991.050.29
Next Step Prepare to Evaluate
V0=27501.22991.050.29
Next Step Evaluate
V0=6.79877570892459m/s
LAST Step Rounding Answer
V0=6.7988m/s

Velocity at Sea-Level given Lift Coefficient Formula Elements

Variables
Constants
Functions
Velocity at Sea-Level
Velocity at Sea-Level is the distance traveled per unit of time by aircraft at sea-level conditions.
Symbol: V0
Measurement: SpeedUnit: m/s
Note: Value can be positive or negative.
Weight of Body
Weight of Body is the force acting on the object due to gravity.
Symbol: Wbody
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Reference Area
The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.
Symbol: S
Measurement: AreaUnit:
Note: Value should be greater than 0.
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: CL
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Standard air density at sea-level conditions
Standard air density at sea-level conditions represents the mass of air per unit volume under standard atmospheric conditions.
Symbol: [Std-Air-Density-Sea]
Value: 1.229
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 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
​Go Velocity at Altitude given Velocity at Sea-Level
Valt=V0[Std-Air-Density-Sea]ρ0

How to Evaluate Velocity at Sea-Level given Lift Coefficient?

Velocity at Sea-Level given Lift Coefficient evaluator uses Velocity at Sea-Level = sqrt((2*Weight of Body)/([Std-Air-Density-Sea]*Reference Area*Lift Coefficient)) to evaluate the Velocity at Sea-Level, Velocity at Sea-Level given Lift Coefficient is a measure that calculates the velocity of an object at sea level, taking into account the body weight, air density at sea level, reference area and lift coefficient, providing a crucial parameter in aerodynamics and aircraft design. Velocity at Sea-Level is denoted by V0 symbol.

How to evaluate Velocity at Sea-Level given Lift Coefficient using this online evaluator? To use this online evaluator for Velocity at Sea-Level given Lift Coefficient, enter Weight of Body (Wbody), Reference Area (S) & Lift Coefficient (CL) and hit the calculate button.

FAQs on Velocity at Sea-Level given Lift Coefficient

What is the formula to find Velocity at Sea-Level given Lift Coefficient?
The formula of Velocity at Sea-Level given Lift Coefficient is expressed as Velocity at Sea-Level = sqrt((2*Weight of Body)/([Std-Air-Density-Sea]*Reference Area*Lift Coefficient)). Here is an example- 6.798776 = sqrt((2*750)/([Std-Air-Density-Sea]*91.05*0.29)).
How to calculate Velocity at Sea-Level given Lift Coefficient?
With Weight of Body (Wbody), Reference Area (S) & Lift Coefficient (CL) we can find Velocity at Sea-Level given Lift Coefficient using the formula - Velocity at Sea-Level = sqrt((2*Weight of Body)/([Std-Air-Density-Sea]*Reference Area*Lift Coefficient)). This formula also uses Standard air density at sea-level conditions constant(s) and Square Root (sqrt) function(s).
Can the Velocity at Sea-Level given Lift Coefficient be negative?
Yes, the Velocity at Sea-Level given Lift Coefficient, measured in Speed can be negative.
Which unit is used to measure Velocity at Sea-Level given Lift Coefficient?
Velocity at Sea-Level given Lift Coefficient 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 Velocity at Sea-Level given Lift Coefficient can be measured.
Copied!