Velocity for given pull-up maneuver rate Calculator

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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%

✖Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.ⓘ Velocity for given pull-up maneuver rate [v]

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Formula

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Velocity for given pull-up maneuver rate

Formula

`"v" = "[g]"*("n"-1)/"ω"`

Example

`"98.57538m/s"="[g]"*("1.2"-1)/"1.14degree/s"`

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Velocity for given pull-up maneuver rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Velocity - (Measured in Meter per Second) - Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.
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: 1.14 Degree per Second --> 0.0198967534727316 Radian per Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

v = [g]*(n-1)/ω --> [g]*(1.2-1)/0.0198967534727316

Evaluating ... ...

v = 98.5753782740482

STEP 3: Convert Result to Output's Unit

98.5753782740482 Meter per Second --> No Conversion Required

FINAL ANSWER

98.5753782740482 ≈ 98.57538 Meter per Second <-- 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])

Change in Angle of Attack due to Upward Gust

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

Load Factor given Pull-down Maneuver Radius

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

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)

Velocity for given pull-up maneuver rate

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

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

Velocity = [g]*(Load factor-1)/Turn Rate
v = [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 Velocity = [g]*(Load factor-1)/Turn Rate to calculate the Velocity, The Velocity for given pull-up maneuver rate is a function of the aircraft's load factor and maneuver rate. Velocity is denoted by v 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 -> 37.45864 = [g]*(1.2-1)/0.0198967534727316.

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 = [g]*(n-1)/ω or 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 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.

How many ways are there to calculate Velocity?

In this formula, Velocity uses Load factor & Turn Rate. We can use 5 other way(s) to calculate the same, which is/are as follows -

Velocity = sqrt(Turn Radius*Load factor*[g])
Velocity = sqrt(Turn Radius*[g]*(Load factor-1))
Velocity = sqrt(Turn Radius*[g]*(Load factor+1))
Velocity = [g]*(1+Load factor)/Turn Rate
Velocity = [g]*Load factor/Turn Rate

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