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

✖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 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 given turn rate for high-performance fighter aircraft [n]

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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*ω/[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: 589.15 Meter per Second --> 589.15 Meter per Second No Conversion Required
Turn Rate: 1.144 Degree per Second --> 0.0199665666428114 Radian per Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

n = v*ω/[g] --> 589.15*0.0199665666428114/[g]

Evaluating ... ...

n = 1.19952305197109

STEP 3: Convert Result to Output's Unit

1.19952305197109 --> No Conversion Required

FINAL ANSWER

1.19952305197109 ≈ 1.199523 <-- Load Factor

(Calculation completed in 00.011 seconds)

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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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< High Load Factor Maneuver Calculators

Velocity given Turn Radius for High Load Factor

LaTeX Go Velocity = sqrt(Turn Radius*Load Factor*[g])

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

LaTeX Go Load Factor = (Velocity^2)/([g]*Turn Radius)

Turn radius for high load factor

LaTeX Go Turn Radius = (Velocity^2)/([g]*Load Factor)

Turn Rate for High Load Factor

LaTeX Go Turn Rate = [g]*Load Factor/Velocity

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

LaTeX Go

Load Factor = Velocity*Turn Rate/[g]
n = v*ω/[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 represents the ratio of the lift force to the weight of the aircraft, it indicates the magnitude of the forces experienced by the aircraft during maneuvers, this equation suggests that the load factor experienced by the aircraft during a turn is directly proportional to the product of the velocity and the turn rate, and inversely proportional to the gravitational acceleration. 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 (ω) 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 -> 0.488646 = 589.15*0.0199665666428114/[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 represents the ratio of the lift force to the weight of the aircraft, it indicates the magnitude of the forces experienced by the aircraft during maneuvers, this equation suggests that the load factor experienced by the aircraft during a turn is directly proportional to the product of the velocity and the turn rate, and inversely proportional to the gravitational acceleration and is represented as n = v*ω/[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 represents the ratio of the lift force to the weight of the aircraft, it indicates the magnitude of the forces experienced by the aircraft during maneuvers, this equation suggests that the load factor experienced by the aircraft during a turn is directly proportional to the product of the velocity and the turn rate, and inversely proportional to the gravitational acceleration 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 (ω). 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 1 other way(s) to calculate the same, which is/are as follows -

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

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