Load Factor given Pull-Down Maneuver Rate Calculator

✖Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.ⓘ Pull-Down Maneuver Velocity [V_pull-down]			+10% -10%
✖Pull-Down Turn Rate refers to the rate at which an aircraft executes a pull down maneuver.ⓘ Pull-Down Turn Rate [ω_pull-down]			+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-Down Maneuver Rate [n]

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Load Factor given Pull-Down Maneuver Rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1
n = ((V_pull-down*ω_pull-down)/[g])-1
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-Down Maneuver Velocity - (Measured in Meter per Second) - Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.
Pull-Down Turn Rate - (Measured in Radian per Second) - Pull-Down Turn Rate refers to the rate at which an aircraft executes a pull down maneuver.

STEP 1: Convert Input(s) to Base Unit

Pull-Down Maneuver Velocity: 797.71 Meter per Second --> 797.71 Meter per Second No Conversion Required
Pull-Down Turn Rate: 1.5496 Degree per Second --> 0.027045622088899 Radian per Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

n = ((V_pull-down*ω_pull-down)/[g])-1 --> ((797.71*0.027045622088899)/[g])-1

Evaluating ... ...

n = 1.19999318794243

STEP 3: Convert Result to Output's Unit

1.19999318794243 --> No Conversion Required

FINAL ANSWER

1.19999318794243 ≈ 1.199993 <-- 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-Down Maneuver Rate Formula

LaTeX Go

Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1
n = ((V_pull-down*ω_pull-down)/[g])-1

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Rolling scissors, also called vertical scissors, tend to happen after a high-speed overshoot from above. The defender reverses into a steep climb and a barrel roll over the top, forcing the attacker to attempt to follow.

How to Calculate Load Factor given Pull-Down Maneuver Rate?

Load Factor given Pull-Down Maneuver Rate calculator uses Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1 to calculate the Load Factor, The Load Factor given Pull-Down Maneuver Rate is the measure of the forces experienced by an aircraft during a pull-down maneuver, relative to gravity. This formula calculates the load factor based on the aircraft's velocity during the pull-down maneuver, the pull-down rate, and gravitational acceleration. Understanding and applying this formula is essential for pilots and engineers to evaluate the structural integrity and aerodynamic performance during pull-down maneuvers. Load Factor is denoted by n symbol.

How to calculate Load Factor given Pull-Down Maneuver Rate using this online calculator? To use this online calculator for Load Factor given Pull-Down Maneuver Rate, enter Pull-Down Maneuver Velocity (V_pull-down) & Pull-Down Turn Rate (ω_pull-down) and hit the calculate button. Here is how the Load Factor given Pull-Down Maneuver Rate calculation can be explained with given input values -> 1.199993 = ((797.71*0.027045622088899)/[g])-1.

FAQ

What is Load Factor given Pull-Down Maneuver Rate?

The Load Factor given Pull-Down Maneuver Rate is the measure of the forces experienced by an aircraft during a pull-down maneuver, relative to gravity. This formula calculates the load factor based on the aircraft's velocity during the pull-down maneuver, the pull-down rate, and gravitational acceleration. Understanding and applying this formula is essential for pilots and engineers to evaluate the structural integrity and aerodynamic performance during pull-down maneuvers and is represented as n = ((V_pull-down*ω_pull-down)/[g])-1 or Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1. Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent & Pull-Down Turn Rate refers to the rate at which an aircraft executes a pull down maneuver.

How to calculate Load Factor given Pull-Down Maneuver Rate?

The Load Factor given Pull-Down Maneuver Rate is the measure of the forces experienced by an aircraft during a pull-down maneuver, relative to gravity. This formula calculates the load factor based on the aircraft's velocity during the pull-down maneuver, the pull-down rate, and gravitational acceleration. Understanding and applying this formula is essential for pilots and engineers to evaluate the structural integrity and aerodynamic performance during pull-down maneuvers is calculated using Load Factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1. To calculate Load Factor given Pull-Down Maneuver Rate, you need Pull-Down Maneuver Velocity (V_pull-down) & Pull-Down Turn Rate (ω_pull-down). With our tool, you need to enter the respective value for Pull-Down Maneuver Velocity & Pull-Down 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 Pull-Down Maneuver Velocity & Pull-Down Turn Rate. We can use 2 other way(s) to calculate the same, which is/are as follows -

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

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