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

STEP 0: Pre-Calculation Summary
Formula Used
Load factor = Velocity*Turn Rate/[g]
n = v*ฯ‰/[g]
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 Rate - (Measured in Radian per Second) - Turn Rate is the rate at which an aircraft executes a turn expressed in degrees per second.
STEP 1: Convert Input(s) to Base Unit
Velocity: 60 Meter per Second --> 60 Meter per Second No Conversion Required
Turn Rate: 1.14 Degree per Second --> 0.0198967534727316 Radian per Second (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
n = v*ฯ‰/[g] --> 60*0.0198967534727316/[g]
Evaluating ... ...
n = 0.121734252610616
STEP 3: Convert Result to Output's Unit
0.121734252610616 --> No Conversion Required
FINAL ANSWER
0.121734252610616 โ‰ˆ 0.121734 <-- Load factor
(Calculation completed in 00.004 seconds)

Credits

Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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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 rate for high-performance fighter aircraft Formula

Load factor = Velocity*Turn Rate/[g]
n = v*ฯ‰/[g]

What is a defensive split?

A pair of fighters encountering one or two attackers will often use a defensive split. The maneuver consists of both defenders making turns in opposite directions, forcing the attackers to follow only one aircraft. This allows the other defender to circle and maneuver behind the attackers.

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

Load factor for given turn rate for high-performance fighter aircraft calculator uses Load factor = Velocity*Turn Rate/[g] to calculate the Load factor, The Load factor for given turn rate for high-performance fighter aircraft depends on the aircraft's velocity and turn rate. Load factor is denoted by n symbol.

How to calculate Load factor for given turn rate for high-performance fighter aircraft using this online calculator? To use this online calculator for Load factor for given turn rate for high-performance fighter aircraft, enter Velocity (v) & Turn Rate (ฯ‰) and hit the calculate button. Here is how the Load factor for given turn rate for high-performance fighter aircraft calculation can be explained with given input values -> 0.320353 = 60*0.0198967534727316/[g].

FAQ

What is Load factor for given turn rate for high-performance fighter aircraft?
The Load factor for given turn rate for high-performance fighter aircraft depends on the aircraft's velocity and turn rate and is represented as n = v*ฯ‰/[g] or Load factor = Velocity*Turn Rate/[g]. 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 Rate is the rate at which an aircraft executes a turn expressed in degrees per second.
How to calculate Load factor for given turn rate for high-performance fighter aircraft?
The Load factor for given turn rate for high-performance fighter aircraft depends on the aircraft's velocity and turn rate is calculated using Load factor = Velocity*Turn Rate/[g]. To calculate Load factor for given turn rate for high-performance fighter aircraft, you need Velocity (v) & Turn Rate (ฯ‰). With our tool, you need to enter the respective value for Velocity & Turn Rate 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 Rate. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Load factor = (Velocity^2)/([g]*Turn Radius)
  • 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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