Velocity for given pull-up maneuver rate Calculator

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Aircraft Performance

Aircraft Design

Introduction and Governing Equations

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High Load Factor Maneuver

Pull Up and Pull Down Maneuver

✖Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.ⓘ Load factor [n]			+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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Formula

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Velocity for given pull-up maneuver rate

Formula

`"V"_{"pull-up"} = "[g]"*("n"-1)/"ω"`

Example

`"98.23071m/s"="[g]"*("1.2"-1)/"1.144degree/s"`

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Velocity for given pull-up maneuver rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pull-Up Maneuver Velocity = [g]*(Load factor-1)/Turn Rate
V_pull-up = [g]*(n-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.
Load factor - Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
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

Load factor: 1.2 --> 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-1)/ω --> [g]*(1.2-1)/0.0199665666428114

Evaluating ... ...

V_pull-up = 98.2307091192436

STEP 3: Convert Result to Output's Unit

98.2307091192436 Meter per Second --> No Conversion Required

FINAL ANSWER

98.2307091192436 ≈ 98.23071 Meter per Second <-- Pull-Up Maneuver Velocity

(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!

< 25 High Load Factor Maneuver Calculators

Turn rate for given lift coefficient

Go Turn Rate = [g]*(sqrt((Reference Area*Freestream density*Lift Coefficient*Load factor)/(2*Aircraft weight)))

Turn rate for given wing loading

Go Turn Rate = [g]*(sqrt(Freestream density*Lift Coefficient*Load factor/(2*Wing Loading)))

Lift Coefficient for given turn rate

Go Lift Coefficient = 2*Aircraft weight*(Turn Rate^2)/(([g]^2)*Freestream density*Load factor*Reference Area)

Lift Coefficient for given Turn Radius

Go Lift Coefficient = Aircraft weight/(0.5*Freestream density*Reference Area*[g]*Turn Radius)

Radius of turn for given lift coefficient

Go Turn Radius = 2*Aircraft weight/(Freestream density*Reference Area*[g]*Lift Coefficient)

Wing loading for given turn rate

Go Wing Loading = ([g]^2)*Freestream density*Lift Coefficient*Load factor/(2*(Turn Rate^2))

Lift Coefficient for given wing loading and turn radius

Go Lift Coefficient = 2*Wing Loading/(Freestream density*Turn Radius*[g])

Radius of turn for given wing loading

Go Turn Radius = 2*Wing Loading/(Freestream density*Lift Coefficient*[g])

Wing loading for given turn radius

Go Wing Loading = (Turn Radius*Freestream density*Lift Coefficient*[g])/2

Velocity for given pull-up maneuver radius

Go Velocity = sqrt(Turn Radius*[g]*(Load factor-1))

Velocity given Pull-down Maneuver Radius

Go Velocity = sqrt(Turn Radius*[g]*(Load factor+1))

Velocity given Turn Radius for High Load Factor

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

Load Factor given Pull-down Maneuver Radius

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

Change in Angle of Attack due to Upward Gust

Go Change in Angle of Attack = tan(Gust Velocity/Flight Velocity)

Velocity for given pull-up maneuver rate

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

Load Factor given Pull-UP Maneuver Radius

Go Load factor = 1+((Velocity^2)/(Turn Radius*[g]))

Pull-down maneuver radius

Go Turn Radius = (Velocity^2)/([g]*(Load factor+1))

Pull-up maneuver radius

Go Turn Radius = (Velocity^2)/([g]*(Load factor-1))

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

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

Turn radius for high load factor

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

Load Factor given Pull-Up Maneuver Rate

Go Load factor = 1+(Velocity*Turn Rate/[g])

Pull-down maneuver rate

Go Turn Rate = [g]*(1+Load factor)/Velocity

Pull-up maneuver rate

Go Turn Rate = [g]*(Load factor-1)/Velocity

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

Go Load factor = Velocity*Turn Rate/[g]

Turn rate for high load factor

Go Turn Rate = [g]*Load factor/Velocity

Velocity for given pull-up maneuver rate Formula

Pull-Up Maneuver Velocity = [g]*(Load factor-1)/Turn Rate
V_pull-up = [g]*(n-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]*(Load factor-1)/Turn Rate to calculate the Pull-Up Maneuver Velocity, The Velocity for given pull-up maneuver rate is a function of the aircraft's load factor and maneuver rate. 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 Load factor (n) & 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 -> 98.23071 = [g]*(1.2-1)/0.0199665666428114.

FAQ

What is Velocity for given pull-up maneuver rate?

The Velocity for given pull-up maneuver rate is a function of the aircraft's load factor and maneuver rate and is represented as V_pull-up = [g]*(n-1)/ω or Pull-Up Maneuver Velocity = [g]*(Load factor-1)/Turn Rate. Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft & 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 a function of the aircraft's load factor and maneuver rate is calculated using Pull-Up Maneuver Velocity = [g]*(Load factor-1)/Turn Rate. To calculate Velocity for given pull-up maneuver rate, you need Load factor (n) & Turn Rate (ω). With our tool, you need to enter the respective value for 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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