Load Factor given Pull-UP Maneuver Radius Calculator

✖Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent.ⓘ Pull-Up Maneuver Velocity [V_pull-up]			+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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Load Factor given Pull-UP Maneuver Radius Solution

STEP 0: Pre-Calculation Summary

Formula Used

Load Factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g]))
n = 1+((V_pull-up^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.
Pull-Up Maneuver Velocity - (Measured in Meter per Second) - Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent.
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

Pull-Up Maneuver Velocity: 240.52 Meter per Second --> 240.52 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 = 1+((V_pull-up^2)/(R*[g])) --> 1+((240.52^2)/(29495.25*[g]))

Evaluating ... ...

n = 1.19999983307669

STEP 3: Convert Result to Output's Unit

1.19999983307669 --> No Conversion Required

FINAL ANSWER

1.19999983307669 ≈ 1.2 <-- Load Factor

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

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

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< Pull Up and Pull Down Maneuver Calculators

Velocity for given Pull-Up Maneuver Radius

LaTeX Go Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1))

Load Factor given Pull-UP Maneuver Radius

LaTeX Go Load Factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g]))

Pull-up maneuver radius

LaTeX Go Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1))

Pull-Up Maneuver Rate

LaTeX Go Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity

Load Factor given Pull-UP Maneuver Radius Formula

LaTeX Go

Load Factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g]))
n = 1+((V_pull-up^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+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])) to calculate the Load Factor, The Load Factor given Pull-up Maneuver Radius measures the gravitational force multiples experienced by an aircraft during a pull-up maneuver. This formula calculates the load factor based on the square of the velocity during the pull-up maneuver, the turn radius, and gravitational acceleration. 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 Pull-Up Maneuver Velocity (V_pull-up) & 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 -> 1.2 = 1+((240.52^2)/(29495.25*[g])).

FAQ

What is Load Factor given Pull-UP Maneuver Radius?

The Load Factor given Pull-up Maneuver Radius measures the gravitational force multiples experienced by an aircraft during a pull-up maneuver. This formula calculates the load factor based on the square of the velocity during the pull-up maneuver, the turn radius, and gravitational acceleration and is represented as n = 1+((V_pull-up^2)/(R*[g])) or Load Factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])). Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent & 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 measures the gravitational force multiples experienced by an aircraft during a pull-up maneuver. This formula calculates the load factor based on the square of the velocity during the pull-up maneuver, the turn radius, and gravitational acceleration is calculated using Load Factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])). To calculate Load Factor given Pull-UP Maneuver Radius, you need Pull-Up Maneuver Velocity (V_pull-up) & Turn Radius (R). With our tool, you need to enter the respective value for Pull-Up Maneuver 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 Pull-Up Maneuver Velocity & Turn Radius. We can use 2 other way(s) to calculate the same, which is/are as follows -

Load Factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1
Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1

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