Pull-Up Maneuver Rate Calculator

✖Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver.ⓘ Pull-Up Load Factor [n_pull-up]			+10% -10%
✖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 Rate is the rate at which an aircraft executes a turn expressed in degrees per second.ⓘ Pull-Up Maneuver Rate [ω]

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Pull-Up Maneuver Rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity
ω = [g]*(n_pull-up-1)/V_pull-up
This formula uses 1 Constants, 3 Variables

Constants Used

[g] - Gravitational acceleration on Earth Value Taken As 9.80665

Variables Used

Turn Rate - (Measured in Radian per Second) - Turn Rate is the rate at which an aircraft executes a turn expressed in degrees per second.
Pull-Up Load Factor - Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver.
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.

STEP 1: Convert Input(s) to Base Unit

Pull-Up Load Factor: 1.489 --> No Conversion Required
Pull-Up Maneuver Velocity: 240.52 Meter per Second --> 240.52 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

ω = [g]*(n_pull-up-1)/V_pull-up --> [g]*(1.489-1)/240.52

Evaluating ... ...

ω = 0.0199378506984866

STEP 3: Convert Result to Output's Unit

0.0199378506984866 Radian per Second -->1.14235469758546 Degree per Second (Check conversion here)

FINAL ANSWER

1.14235469758546 ≈ 1.142355 Degree per Second <-- Turn Rate

(Calculation completed in 00.004 seconds)

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Credits

Created by Vinay Mishra

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

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

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< 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

Pull-Up Maneuver Rate Formula

LaTeX Go

Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity
ω = [g]*(n_pull-up-1)/V_pull-up

What are aerobatic maneuvers?

Aerobatic maneuvers are flight paths putting aircraft in unusual attitudes, in air shows, dogfights, or competition aerobatics.

How to Calculate Pull-Up Maneuver Rate?

Pull-Up Maneuver Rate calculator uses Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity to calculate the Turn Rate, The Pull-up Maneuver Rate quantifies the rate at which an aircraft ascends during a pull-up maneuver. This formula calculates the turn rate based on gravitational acceleration, the load factor during the pull-up maneuver, and the velocity during the pull-up. Understanding and applying this formula is crucial for pilots and engineers to optimize the ascent rate. Turn Rate is denoted by ω symbol.

How to calculate Pull-Up Maneuver Rate using this online calculator? To use this online calculator for Pull-Up Maneuver Rate, enter Pull-Up Load Factor (n_pull-up) & Pull-Up Maneuver Velocity (V_pull-up) and hit the calculate button. Here is how the Pull-Up Maneuver Rate calculation can be explained with given input values -> 64.24746 = [g]*(1.489-1)/240.52.

FAQ

What is Pull-Up Maneuver Rate?

The Pull-up Maneuver Rate quantifies the rate at which an aircraft ascends during a pull-up maneuver. This formula calculates the turn rate based on gravitational acceleration, the load factor during the pull-up maneuver, and the velocity during the pull-up. Understanding and applying this formula is crucial for pilots and engineers to optimize the ascent rate and is represented as ω = [g]*(n_pull-up-1)/V_pull-up or Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity. Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver & Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent.

How to calculate Pull-Up Maneuver Rate?

The Pull-up Maneuver Rate quantifies the rate at which an aircraft ascends during a pull-up maneuver. This formula calculates the turn rate based on gravitational acceleration, the load factor during the pull-up maneuver, and the velocity during the pull-up. Understanding and applying this formula is crucial for pilots and engineers to optimize the ascent rate is calculated using Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity. To calculate Pull-Up Maneuver Rate, you need Pull-Up Load Factor (n_pull-up) & Pull-Up Maneuver Velocity (V_pull-up). With our tool, you need to enter the respective value for Pull-Up Load Factor & Pull-Up Maneuver Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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