Load Factor given Pull-UP Maneuver Radius Calculator

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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 given Pull-UP Maneuver Radius [n]

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Formula

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Load Factor given Pull-UP Maneuver Radius

Formula

`"n" = 1+(("v"^2)/("R"*"[g]"))`

Example

`"2.223659"=1+((("60m/s")^2)/("300m"*"[g]"))`

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Load Factor given Pull-UP Maneuver Radius Solution

STEP 0: Pre-Calculation Summary

Formula Used

Load factor = 1+((Velocity^2)/(Turn Radius*[g]))
n = 1+((v^2)/(R*[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 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 = 1+((v^2)/(R*[g])) --> 1+((60^2)/(300*[g]))

Evaluating ... ...

n = 2.22365945557351

STEP 3: Convert Result to Output's Unit

2.22365945557351 --> No Conversion Required

FINAL ANSWER

2.22365945557351 ≈ 2.223659 <-- Load factor

(Calculation completed in 00.006 seconds)

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Home » Physics » Aircraft Mechanics » Aircraft Performance » Maneuvering Flight » High Load Factor Maneuver » Load Factor given Pull-UP Maneuver Radius

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Created by Vinay Mishra

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

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Verified by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad

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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 given Pull-UP Maneuver Radius Formula

Load factor = 1+((Velocity^2)/(Turn Radius*[g]))
n = 1+((v^2)/(R*[g]))

What are basic fighter maneuvers?

Basic fighter maneuvers (BFM) are used by fighter pilots during a dogfight to gain a positional advantage over an opponent. Pilots must have a keen knowledge of not only their own aircraft's performance characteristics but also of the opponents, taking advantage of their own strengths while exploiting the enemy's weaknesses.

How to Calculate Load Factor given Pull-UP Maneuver Radius?

Load Factor given Pull-UP Maneuver Radius calculator uses Load factor = 1+((Velocity^2)/(Turn Radius*[g])) to calculate the Load factor, The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius. Load factor is denoted by n symbol.

How to calculate Load Factor given Pull-UP Maneuver Radius using this online calculator? To use this online calculator for Load Factor given Pull-UP Maneuver Radius, enter Velocity (v) & Turn Radius (R) and hit the calculate button. Here is how the Load Factor given Pull-UP Maneuver Radius calculation can be explained with given input values -> 2.223659 = 1+((60^2)/(300*[g])).

FAQ

What is Load Factor given Pull-UP Maneuver Radius?

The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius and is represented as n = 1+((v^2)/(R*[g])) or Load factor = 1+((Velocity^2)/(Turn Radius*[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 Radius is the radius of the flight path causing the airplane to turn in a circular path.

How to calculate Load Factor given Pull-UP Maneuver Radius?

The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius is calculated using Load factor = 1+((Velocity^2)/(Turn Radius*[g])). To calculate Load Factor given Pull-UP Maneuver Radius, 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^2)/([g]*Turn Radius)
Load factor = Velocity*Turn Rate/[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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