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Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft. Check FAQs
n=FLW
n - Load Factor?FL - Lift Force?W - Aircraft Weight?

Load factor given Lift Force and Weight of Aircraft Example

With values
With units
Only example

Here is how the Load factor given Lift Force and Weight of Aircraft equation looks like with Values.

Here is how the Load factor given Lift Force and Weight of Aircraft equation looks like with Units.

Here is how the Load factor given Lift Force and Weight of Aircraft equation looks like.

1.1111Edit=20Edit18Edit
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Load factor given Lift Force and Weight of Aircraft Solution

Follow our step by step solution on how to calculate Load factor given Lift Force and Weight of Aircraft?

FIRST Step Consider the formula
n=FLW
Next Step Substitute values of Variables
n=20N18N
Next Step Prepare to Evaluate
n=2018
Next Step Evaluate
n=1.11111111111111
LAST Step Rounding Answer
n=1.1111

Load factor given Lift Force and Weight of Aircraft Formula Elements

Variables
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.
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.
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 Load Factor

​Go Load Factor given Turn Rate
n=(Vω[g])2+1
​Go Load Factor given Turn Radius
n=1+(V2[g]R)2

Other formulas in Turning Flight category

​Go Velocity for given turn rate
V=[g]n2-1ω
​Go Turn rate
ω=[g]n2-1V
​Go Lift for given Load Factor
FL=nW
​Go Weight for given Load Factor
W=FLn

How to Evaluate Load factor given Lift Force and Weight of Aircraft?

Load factor given Lift Force and Weight of Aircraft evaluator uses Load Factor = Lift Force/Aircraft Weight to evaluate the Load Factor, Load Factor Given Lift Force and Weight of Aircraft is a measure that quantifies the stress imposed on an aircraft during turns, calculated by dividing the lift force generated during a turn by the weight of the aircraft, providing a critical metric for aircraft performance and safety analysis. Load Factor is denoted by n symbol.

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

FAQs on Load factor given Lift Force and Weight of Aircraft

What is the formula to find Load factor given Lift Force and Weight of Aircraft?
The formula of Load factor given Lift Force and Weight of Aircraft is expressed as Load Factor = Lift Force/Aircraft Weight. Here is an example- 1.111111 = 20/18.
How to calculate Load factor given Lift Force and Weight of Aircraft?
With Lift Force (FL) & Aircraft Weight (W) we can find Load factor given Lift Force and Weight of Aircraft using the formula - Load Factor = Lift Force/Aircraft Weight.
What are the other ways to Calculate Load Factor?
Here are the different ways to Calculate Load Factor-
  • Load Factor=sqrt((Flight Velocity*Turn Rate/[g])^2+1)OpenImg
  • Load Factor=sqrt(1+(Flight Velocity^2/([g]*Turn Radius))^2)OpenImg
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