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

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

✖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 Rate is the rate at which an aircraft executes a turn expressed in degrees per secondⓘ Turn Rate [ω]			+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 turn rate for a high-performance fighter aircraft [n]

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Vinay Mishra

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

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

Shikha Maurya

Indian Institute of Technology (IIT), Bombay

Shikha Maurya has verified this Calculator and 100+ more calculators!

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< 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 pull-up maneuver radius

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

Load factor=Lift force/Weight GO

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

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

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

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Radius of turn for a given lift coefficient GO

Lift Coefficient for a given turn radius GO

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Lift Coefficient for a given turn rate GO

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Lift Coefficient for a given wing loading and turn radius GO

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Wing loading for a given turn rate GO

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 a given turn rate for a high-performance fighter aircraft?

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

How to calculate Load factor for a given turn rate for a high-performance fighter aircraft using this online calculator? To use this online calculator for Load factor for a given turn rate for a high-performance fighter aircraft, enter Velocity (v) and Turn Rate (ω) and hit the calculate button. Here is how the Load factor for a given turn rate for a high-performance fighter aircraft calculation can be explained with given input values -> 0.320353 = 60*0.05235987755982/[g].

FAQ

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

The Load factor for a given turn rate for a high-performance fighter aircraft depends on the aircraft's velocity and turn rate and is represented as n=v*ω/[g] or Load factor=Velocity*Turn Rate/[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 Rate is the rate at which an aircraft executes a turn expressed in degrees per second.

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

The Load factor for a given turn rate for a 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 a given turn rate for a high-performance fighter aircraft, you need Velocity (v) and Turn Rate (ω). With our tool, you need to enter the respective value for Velocity and 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 and Turn Rate. 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^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
Load factor=(Velocity^2)/([g]*Turn Radius)

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