Velocity for given 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%
✖Turn Rate is the rate at which an aircraft executes a turn expressed in degrees per second.ⓘ Turn Rate [ω]			+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.ⓘ Velocity for given pull-up maneuver rate [V_pull-up]

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Velocity for given pull-up maneuver rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Constants Used

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

Variables Used

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.
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.
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

Pull-Up Load Factor: 1.489 --> 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

V_pull-up = [g]*(n_pull-up-1)/ω --> [g]*(1.489-1)/0.0199665666428114

Evaluating ... ...

V_pull-up = 240.174083796551

STEP 3: Convert Result to Output's Unit

240.174083796551 Meter per Second --> No Conversion Required

FINAL ANSWER

240.174083796551 ≈ 240.1741 Meter per Second <-- Pull-Up Maneuver Velocity

(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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< 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

Velocity for given pull-up maneuver rate Formula

LaTeX Go

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

What is a spin?

A spin is more complex, intentionally stalling a single wing, causing the plane to descend, spiraling around its yaw axis in a corkscrew motion.

How to Calculate Velocity for given pull-up maneuver rate?

Velocity for given pull-up maneuver rate calculator uses Pull-Up Maneuver Velocity = [g]*(Pull-Up Load Factor-1)/Turn Rate to calculate the Pull-Up Maneuver Velocity, The Velocity for given Pull-up Maneuver Rate is the speed required for an aircraft to maintain a specific rate of ascent during a pull-up maneuver. This formula calculates the velocity based on gravitational acceleration, the pull-up load factor, and the turn rate. Understanding and applying this formula is essential for pilots and engineers to ensure safe and effective pull-up maneuvers. Pull-Up Maneuver Velocity is denoted by V_pull-up symbol.

How to calculate Velocity for given pull-up maneuver rate using this online calculator? To use this online calculator for Velocity for given pull-up maneuver rate, enter Pull-Up Load Factor (n_pull-up) & Turn Rate (ω) and hit the calculate button. Here is how the Velocity for given pull-up maneuver rate calculation can be explained with given input values -> 240.1741 = [g]*(1.489-1)/0.0199665666428114.

FAQ

What is Velocity for given pull-up maneuver rate?

The Velocity for given Pull-up Maneuver Rate is the speed required for an aircraft to maintain a specific rate of ascent during a pull-up maneuver. This formula calculates the velocity based on gravitational acceleration, the pull-up load factor, and the turn rate. Understanding and applying this formula is essential for pilots and engineers to ensure safe and effective pull-up maneuvers and is represented as V_pull-up = [g]*(n_pull-up-1)/ω or Pull-Up Maneuver Velocity = [g]*(Pull-Up Load Factor-1)/Turn Rate. Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver & Turn Rate is the rate at which an aircraft executes a turn expressed in degrees per second.

How to calculate Velocity for given pull-up maneuver rate?

The Velocity for given Pull-up Maneuver Rate is the speed required for an aircraft to maintain a specific rate of ascent during a pull-up maneuver. This formula calculates the velocity based on gravitational acceleration, the pull-up load factor, and the turn rate. Understanding and applying this formula is essential for pilots and engineers to ensure safe and effective pull-up maneuvers is calculated using Pull-Up Maneuver Velocity = [g]*(Pull-Up Load Factor-1)/Turn Rate. To calculate Velocity for given pull-up maneuver rate, you need Pull-Up Load Factor (n_pull-up) & Turn Rate (ω). With our tool, you need to enter the respective value for Pull-Up Load Factor & Turn Rate 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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