Load factor for a given pull-up maneuver radius Calculator

Category	Physics ↺
Physics	Flight Stability and Control ↺
Flight-Stability-And-Control	Airplane Performance ↺
Airplane-Performance	Maneuvering Flight ↺

✖Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). ⓘ 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 a given pull-up maneuver radius [n]

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Load factor for a given pull-up maneuver radius

Vinay Mishra

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

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

Sai Venkata Phanindra Chary Arendra

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

Sai Venkata Phanindra Chary Arendra has verified this Calculator and 100+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Air Resistance Force

Air Resistance=Air Constant*Velocity^2 GO

Archimedes Principle

Archimedes Principle=Density*Acceleration Due To Gravity*Velocity GO

Wavelength Of The Wave(Using Velocity)

Wavelength Of A Wave=Velocity*Time Period Of Progressive Wave GO

Time Period (Using Velocity )

Time Period Of Progressive Wave=Wavelength/Velocity GO

Stokes Force

Stokes Force=6*pi*Radius*Dynamic viscosity*Velocity GO

Angular Frequency (Using Velocity )

Angular Frequency=(2*pi*Velocity)/Wavelength GO

Centripetal Force

Centripetal Force=(Mass*(Velocity)^2)/Radius GO

Frequency Of Wavelength ( Using Velocity )

frequency=Velocity/Wavelength Of A Wave GO

Wave Number (Using Angular Frequency)

Wave Number=Angular Frequency/Velocity GO

Kinetic Energy

Kinetic Energy=(Mass*Velocity^2)/2 GO

Wavelength Of The Wave(Using Frequency)

Wavelength=Velocity/frequency GO

< 8 Other formulas that calculate the same Output

Load factor for a given turn radius

Load factor=sqrt(1+(((Velocity^2)/([g]*Turn Radius))^2)) GO

Load factor for a given turn rate

Load factor=sqrt(((Velocity*Turn Rate/[g])^2)+1) GO

Load factor for a given pull-down maneuver radius

Load factor=((Velocity^2)/(Turn Radius*[g]))-1 GO

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

Load factor=(Velocity^2)/([g]*Turn Radius) GO

Load factor for a given pull-down maneuver rate

Load factor=((Velocity*Turn Rate)/[g])-1 GO

Load factor for a given pull-up maneuver rate

Load factor=1+(Velocity*Turn Rate/[g]) GO

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

Load factor=Velocity*Turn Rate/[g] GO

Load factor

Load factor=Lift force/Weight GO

Load factor for a given pull-up maneuver radius Formula

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

More formulas

Pull-up maneuver radius GO

Velocity for a given pull-up maneuver radius GO

Pull-up maneuver rate GO

Load factor for a given pull-up maneuver rate GO

Velocity for a given pull-up maneuver rate GO

Pull-down maneuver radius GO

Velocity for a given pull-down maneuver radius GO

Load factor for a given pull-down maneuver radius GO

Pull-down maneuver rate GO

Velocity for a given pull-down maneuver rate GO

Load factor for a given pull-down maneuver rate GO

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 for a given pull-up maneuver radius?

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

How to calculate Load factor for a given pull-up maneuver radius using this online calculator? To use this online calculator for Load factor for a given pull-up maneuver radius, enter Velocity (v) and Turn Radius (R) and hit the calculate button. Here is how the Load factor for a 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 for a given pull-up maneuver radius?

The Load factor for a 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, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). and Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.

How to calculate Load factor for a given pull-up maneuver radius?

The Load factor for a 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 for a given pull-up maneuver radius, you need Velocity (v) and Turn Radius (R). With our tool, you need to enter the respective value for Velocity and 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 and Turn Radius. We can use 8 other way(s) to calculate the same, which is/are as follows -

Load factor=Lift force/Weight
Load factor=sqrt(1+(((Velocity^2)/([g]*Turn Radius))^2))
Load factor=sqrt(((Velocity*Turn Rate/[g])^2)+1)
Load factor=1+(Velocity*Turn Rate/[g])
Load factor=((Velocity^2)/(Turn Radius*[g]))-1
Load factor=((Velocity*Turn Rate)/[g])-1
Load factor=(Velocity^2)/([g]*Turn Radius)
Load factor=Velocity*Turn Rate/[g]

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