Load factor for given turn radius for high-performance fighter aircraft Solution

STEP 0: Pre-Calculation Summary
Formula Used
Load factor = (Velocity^2)/([g]*Turn Radius)
n = (v^2)/([g]*R)
This formula uses 1 Constants, 3 Variables
Constants Used
[g] - Gravitational acceleration on Earth Value Taken As 9.80665
Variables Used
Load factor - Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
Velocity - (Measured in Meter per Second) - Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.
Turn Radius - (Measured in Meter) - Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
STEP 1: Convert Input(s) to Base Unit
Velocity: 60 Meter per Second --> 60 Meter per Second No Conversion Required
Turn Radius: 300 Meter --> 300 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
n = (v^2)/([g]*R) --> (60^2)/([g]*300)
Evaluating ... ...
n = 1.22365945557351
STEP 3: Convert Result to Output's Unit
1.22365945557351 --> No Conversion Required
FINAL ANSWER
1.22365945557351 โ‰ˆ 1.223659 <-- Load factor
(Calculation completed in 00.020 seconds)

Credits

Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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PSG College of Technology (PSGCT), Coimbatore
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25 High Load Factor Maneuver Calculators

Turn rate for given lift coefficient
Go Turn Rate = [g]*(sqrt((Reference Area*Freestream density*Lift Coefficient*Load factor)/(2*Aircraft weight)))
Turn rate for given wing loading
Go Turn Rate = [g]*(sqrt(Freestream density*Lift Coefficient*Load factor/(2*Wing Loading)))
Lift Coefficient for given turn rate
Go Lift Coefficient = 2*Aircraft weight*(Turn Rate^2)/(([g]^2)*Freestream density*Load factor*Reference Area)
Lift Coefficient for given Turn Radius
Go Lift Coefficient = Aircraft weight/(0.5*Freestream density*Reference Area*[g]*Turn Radius)
Radius of turn for given lift coefficient
Go Turn Radius = 2*Aircraft weight/(Freestream density*Reference Area*[g]*Lift Coefficient)
Wing loading for given turn rate
Go Wing Loading = ([g]^2)*Freestream density*Lift Coefficient*Load factor/(2*(Turn Rate^2))
Lift Coefficient for given wing loading and turn radius
Go Lift Coefficient = 2*Wing Loading/(Freestream density*Turn Radius*[g])
Radius of turn for given wing loading
Go Turn Radius = 2*Wing Loading/(Freestream density*Lift Coefficient*[g])
Wing loading for given turn radius
Go Wing Loading = (Turn Radius*Freestream density*Lift Coefficient*[g])/2
Velocity for given pull-up maneuver radius
Go Velocity = sqrt(Turn Radius*[g]*(Load factor-1))
Velocity given Pull-down Maneuver Radius
Go Velocity = sqrt(Turn Radius*[g]*(Load factor+1))
Velocity given Turn Radius for High Load Factor
Go Velocity = sqrt(Turn Radius*Load factor*[g])
Change in Angle of Attack due to Upward Gust
Go Change in Angle of Attack = tan(Gust Velocity/Flight Velocity)
Load Factor given Pull-down Maneuver Radius
Go Load factor = ((Velocity^2)/(Turn Radius*[g]))-1
Load Factor given Pull-UP Maneuver Radius
Go Load factor = 1+((Velocity^2)/(Turn Radius*[g]))
Pull-down maneuver radius
Go Turn Radius = (Velocity^2)/([g]*(Load factor+1))
Pull-up maneuver radius
Go Turn Radius = (Velocity^2)/([g]*(Load factor-1))
Load factor for given turn radius for high-performance fighter aircraft
Go Load factor = (Velocity^2)/([g]*Turn Radius)
Turn radius for high load factor
Go Turn Radius = (Velocity^2)/([g]*Load factor)
Velocity for given pull-up maneuver rate
Go Velocity = [g]*(Load factor-1)/Turn Rate
Load Factor given Pull-Up Maneuver Rate
Go Load factor = 1+(Velocity*Turn Rate/[g])
Pull-down maneuver rate
Go Turn Rate = [g]*(1+Load factor)/Velocity
Pull-up maneuver rate
Go Turn Rate = [g]*(Load factor-1)/Velocity
Load factor for given turn rate for high-performance fighter aircraft
Go Load factor = Velocity*Turn Rate/[g]
Turn rate for high load factor
Go Turn Rate = [g]*Load factor/Velocity

Load factor for given turn radius for high-performance fighter aircraft Formula

Load factor = (Velocity^2)/([g]*Turn Radius)
n = (v^2)/([g]*R)

What is the load factor for acrobatic aircrafts?

For acrobatic category airplanes, the load factor varies from โˆ’3.0 to +6.0. The maximum load factors, both positive and negative, applicable to an aircraft are usually specified in the aircraft flight manual.

How to Calculate Load factor for given turn radius for high-performance fighter aircraft?

Load factor for given turn radius for high-performance fighter aircraft calculator uses Load factor = (Velocity^2)/([g]*Turn Radius) to calculate the Load factor, The Load factor for given turn radius for high-performance fighter aircraft depends on the velocity and turn radius. Tighter the turn, the higher the load factor. Load factor is denoted by n symbol.

How to calculate Load factor for given turn radius for high-performance fighter aircraft using this online calculator? To use this online calculator for Load factor for given turn radius for high-performance fighter aircraft, enter Velocity (v) & Turn Radius (R) and hit the calculate button. Here is how the Load factor for given turn radius for high-performance fighter aircraft calculation can be explained with given input values -> 1.223659 = (60^2)/([g]*300).

FAQ

What is Load factor for given turn radius for high-performance fighter aircraft?
The Load factor for given turn radius for high-performance fighter aircraft depends on the velocity and turn radius. Tighter the turn, the higher the load factor and is represented as n = (v^2)/([g]*R) or Load factor = (Velocity^2)/([g]*Turn Radius). Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time & Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
How to calculate Load factor for given turn radius for high-performance fighter aircraft?
The Load factor for given turn radius for high-performance fighter aircraft depends on the velocity and turn radius. Tighter the turn, the higher the load factor is calculated using Load factor = (Velocity^2)/([g]*Turn Radius). To calculate Load factor for given turn radius for high-performance fighter aircraft, you need Velocity (v) & Turn Radius (R). With our tool, you need to enter the respective value for Velocity & Turn Radius and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Load factor?
In this formula, Load factor uses Velocity & Turn Radius. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Load factor = Velocity*Turn Rate/[g]
  • Load factor = 1+((Velocity^2)/(Turn Radius*[g]))
  • Load factor = 1+(Velocity*Turn Rate/[g])
  • Load factor = ((Velocity^2)/(Turn Radius*[g]))-1
  • Load factor = ((Velocity*Turn Rate)/[g])-1
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