Velocity for given Pull-Up Maneuver Radius Calculator

✖Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.ⓘ Turn Radius [R]			+10% -10%
✖Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.ⓘ Load Factor [n]			+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 Radius [V_pull-up]

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Velocity for given Pull-Up Maneuver Radius Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1))
V_pull-up = sqrt(R*[g]*(n-1))
This formula uses 1 Constants, 1 Functions, 3 Variables

Constants Used

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

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

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.
Turn Radius - (Measured in Meter) - Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
Load Factor - Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.

STEP 1: Convert Input(s) to Base Unit

Turn Radius: 29495.25 Meter --> 29495.25 Meter No Conversion Required
Load Factor: 1.2 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V_pull-up = sqrt(R*[g]*(n-1)) --> sqrt(29495.25*[g]*(1.2-1))

Evaluating ... ...

V_pull-up = 240.52010037105

STEP 3: Convert Result to Output's Unit

240.52010037105 Meter per Second --> No Conversion Required

FINAL ANSWER

240.52010037105 ≈ 240.5201 Meter per Second <-- Pull-Up Maneuver Velocity

(Calculation completed in 00.014 seconds)

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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

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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

Velocity for given Pull-Up Maneuver Radius Formula

LaTeX Go

Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1))
V_pull-up = sqrt(R*[g]*(n-1))

At what G Do you pass out?

A typical person can handle about 5 g0 (49 m/s2) (meaning some people might pass out when riding a higher-g roller coaster, which in some cases exceeds this point) before losing consciousness.

How to Calculate Velocity for given Pull-Up Maneuver Radius?

Velocity for given Pull-Up Maneuver Radius calculator uses Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1)) to calculate the Pull-Up Maneuver Velocity, The Velocity for given Pull-Up Maneuver Radius of an aircraft is dependent upon the maneuver radius and load factor of the aircraft, this formula provides a simplified approximation of the velocity needed to maintain the desired descent rate during the pull-up maneuver. Pull-Up Maneuver Velocity is denoted by V_pull-up symbol.

How to calculate Velocity for given Pull-Up Maneuver Radius using this online calculator? To use this online calculator for Velocity for given Pull-Up Maneuver Radius, enter Turn Radius (R) & Load Factor (n) and hit the calculate button. Here is how the Velocity for given Pull-Up Maneuver Radius calculation can be explained with given input values -> 240.5201 = sqrt(29495.25*[g]*(1.2-1)).

FAQ

What is Velocity for given Pull-Up Maneuver Radius?

The Velocity for given Pull-Up Maneuver Radius of an aircraft is dependent upon the maneuver radius and load factor of the aircraft, this formula provides a simplified approximation of the velocity needed to maintain the desired descent rate during the pull-up maneuver and is represented as V_pull-up = sqrt(R*[g]*(n-1)) or Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1)). Turn Radius is the radius of the flight path causing the airplane to turn in a circular path & Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.

How to calculate Velocity for given Pull-Up Maneuver Radius?

The Velocity for given Pull-Up Maneuver Radius of an aircraft is dependent upon the maneuver radius and load factor of the aircraft, this formula provides a simplified approximation of the velocity needed to maintain the desired descent rate during the pull-up maneuver is calculated using Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1)). To calculate Velocity for given Pull-Up Maneuver Radius, you need Turn Radius (R) & Load Factor (n). With our tool, you need to enter the respective value for Turn Radius & Load Factor 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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