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Lift Force is the aerodynamic force exerted on an object, such as an aircraft wing, perpendicular to the oncoming airflow. Check FAQs
FL=nW
FL - Lift Force?n - Load Factor?W - Aircraft Weight?

Lift for given Load Factor Example

With values
With units
Only example

Here is how the Lift for given Load Factor equation looks like with Values.

Here is how the Lift for given Load Factor equation looks like with Units.

Here is how the Lift for given Load Factor equation looks like.

19.98Edit=1.11Edit18Edit
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Lift for given Load Factor Solution

Follow our step by step solution on how to calculate Lift for given Load Factor?

FIRST Step Consider the formula
FL=nW
Next Step Substitute values of Variables
FL=1.1118N
Next Step Prepare to Evaluate
FL=1.1118
LAST Step Evaluate
FL=19.98N

Lift for given Load Factor Formula Elements

Variables
Lift Force
Lift Force is the aerodynamic force exerted on an object, such as an aircraft wing, perpendicular to the oncoming airflow.
Symbol: FL
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Load Factor
Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
Symbol: n
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Aircraft Weight
Aircraft Weight refers to the total mass of an aircraft, including its structure, payload, fuel, and passengers.
Symbol: W
Measurement: ForceUnit: N
Note: Value should be greater than 0.

Other Formulas to find Lift Force

​Go Lift during level turn
FL=Wcos(Φ)

Other formulas in Turning Flight category

​Go Load Factor given Turn Rate
n=(Vω[g])2+1
​Go Velocity for given turn rate
V=[g]n2-1ω
​Go Turn rate
ω=[g]n2-1V
​Go Load Factor given Turn Radius
n=1+(V2[g]R)2

How to Evaluate Lift for given Load Factor?

Lift for given Load Factor evaluator uses Lift Force = Load Factor*Aircraft Weight to evaluate the Lift Force, Lift for Given Load Factor is a measure of the upward force exerted on an aircraft during a turn, which is calculated by multiplying the load factor during a turn by the weight of the aircraft during a turn, providing a critical factor in determining the safety and stability of flight during various maneuvers. Lift Force is denoted by FL symbol.

How to evaluate Lift for given Load Factor using this online evaluator? To use this online evaluator for Lift for given Load Factor, enter Load Factor (n) & Aircraft Weight (W) and hit the calculate button.

FAQs on Lift for given Load Factor

What is the formula to find Lift for given Load Factor?
The formula of Lift for given Load Factor is expressed as Lift Force = Load Factor*Aircraft Weight. Here is an example- 23.4 = 1.11*18.
How to calculate Lift for given Load Factor?
With Load Factor (n) & Aircraft Weight (W) we can find Lift for given Load Factor using the formula - Lift Force = Load Factor*Aircraft Weight.
What are the other ways to Calculate Lift Force?
Here are the different ways to Calculate Lift Force-
  • Lift Force=Aircraft Weight/cos(Bank Angle)OpenImg
Can the Lift for given Load Factor be negative?
No, the Lift for given Load Factor, measured in Force cannot be negative.
Which unit is used to measure Lift for given Load Factor?
Lift for given Load Factor is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Lift for given Load Factor can be measured.
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