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

⤿

Aircraft Performance

Aircraft Design

Introduction and Governing Equations

Static Stability and Control

⤿

⤿

High Load Factor Maneuver

Pull Up and Pull Down Maneuver

✖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.ⓘ Velocity [v]			+10% -10%
✖Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.ⓘ Turn Radius [R]			+10% -10%

✖Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.ⓘ Load factor for given turn radius for high-performance fighter aircraft [n]

⎘ Copy

👎

Formula

✖

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

Formula

`"n" = ("v"^2)/("[g]"*"R")`

Example

`"1.199994"=(("589.15m/s")^2)/("[g]"*"29495.25m")`

Calculator

LaTeX

Reset

👍

Download Physics Formula PDF PDF Image

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: 589.15 Meter per Second --> 589.15 Meter per Second No Conversion Required
Turn Radius: 29495.25 Meter --> 29495.25 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

n = (v^2)/([g]*R) --> (589.15^2)/([g]*29495.25)

Evaluating ... ...

n = 1.19999381297315

STEP 3: Convert Result to Output's Unit

1.19999381297315 --> No Conversion Required

FINAL ANSWER

1.19999381297315 ≈ 1.199994 <-- Load factor

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Aircraft Mechanics » Aircraft Performance » Maneuvering Flight » High Load Factor Maneuver » Load factor for given turn radius for high-performance fighter aircraft

Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< 16 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)))

Minimum Flight Velocity

Go Minimum Flight Velocity = sqrt((Aircraft weight/Aircraft Gross Wing Area)*(2/(Air Density))*(1/Lift Coefficient))

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 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 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)

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 −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 refers to the ratio of the lift force experienced by an aircraft to its weight under certain conditions, typically during maneuvers, the load factor is essential for designing aircraft structures to withstand the additional forces experienced during maneuvers and for understanding the performance capabilities of an aircraft under different flight conditions. 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 -> 0.199136 = (589.15^2)/([g]*29495.25).

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 refers to the ratio of the lift force experienced by an aircraft to its weight under certain conditions, typically during maneuvers, the load factor is essential for designing aircraft structures to withstand the additional forces experienced during maneuvers and for understanding the performance capabilities of an aircraft under different flight conditions 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 refers to the ratio of the lift force experienced by an aircraft to its weight under certain conditions, typically during maneuvers, the load factor is essential for designing aircraft structures to withstand the additional forces experienced during maneuvers and for understanding the performance capabilities of an aircraft under different flight conditions 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 1 other way(s) to calculate the same, which is/are as follows -

Load factor = Velocity*Turn Rate/[g]

Home

FREE PDFs

🔍 Search