Pull-up maneuver radius Solution

STEP 0: Pre-Calculation Summary
Formula Used
Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1))
R = (Vpull-up^2)/([g]*(n-1))
This formula uses 1 Constants, 3 Variables
Constants Used
[g] - Gravitational acceleration on Earth Value Taken As 9.80665
Variables Used
Turn Radius - (Measured in Meter) - Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
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.
STEP 1: Convert Input(s) to Base Unit
Pull-Up Maneuver Velocity: 240.52 Meter per Second --> 240.52 Meter per Second No Conversion Required
Load Factor: 1.2 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
R = (Vpull-up^2)/([g]*(n-1)) --> (240.52^2)/([g]*(1.2-1))
Evaluating ... ...
R = 29495.225382776
STEP 3: Convert Result to Output's Unit
29495.225382776 Meter --> No Conversion Required
FINAL ANSWER
29495.225382776 29495.23 Meter <-- Turn Radius
(Calculation completed in 00.004 seconds)

Credits

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Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
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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

Pull-up maneuver radius Formula

​LaTeX ​Go
Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1))
R = (Vpull-up^2)/([g]*(n-1))

What is split S maneuver?

The Split S is an air combat maneuver mostly used to disengage from combat. To execute a Split S, the pilot half-rolls their aircraft inverted and executes a descending half-loop, resulting in level flight in the opposite direction at a lower altitude.

How to Calculate Pull-up maneuver radius?

Pull-up maneuver radius calculator uses Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1)) to calculate the Turn Radius, The Pull-up maneuver radius refers to the radius of the circle that an aircraft can describe when executing a pull-up maneuver, in aviation, a pull-up maneuver involves the aircraft transitioning from level flight or descent to a climb, typically at a steep angle, the radius of the pull-up maneuver indicates the size of the circle that the aircraft describes during this maneuver. Turn Radius is denoted by R symbol.

How to calculate Pull-up maneuver radius using this online calculator? To use this online calculator for Pull-up maneuver radius, enter Pull-Up Maneuver Velocity (Vpull-up) & Load Factor (n) and hit the calculate button. Here is how the Pull-up maneuver radius calculation can be explained with given input values -> 29495.23 = (240.52^2)/([g]*(1.2-1)).

FAQ

What is Pull-up maneuver radius?
The Pull-up maneuver radius refers to the radius of the circle that an aircraft can describe when executing a pull-up maneuver, in aviation, a pull-up maneuver involves the aircraft transitioning from level flight or descent to a climb, typically at a steep angle, the radius of the pull-up maneuver indicates the size of the circle that the aircraft describes during this maneuver and is represented as R = (Vpull-up^2)/([g]*(n-1)) or Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1)). 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 is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
How to calculate Pull-up maneuver radius?
The Pull-up maneuver radius refers to the radius of the circle that an aircraft can describe when executing a pull-up maneuver, in aviation, a pull-up maneuver involves the aircraft transitioning from level flight or descent to a climb, typically at a steep angle, the radius of the pull-up maneuver indicates the size of the circle that the aircraft describes during this maneuver is calculated using Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load Factor-1)). To calculate Pull-up maneuver radius, you need Pull-Up Maneuver Velocity (Vpull-up) & Load Factor (n). With our tool, you need to enter the respective value for Pull-Up Maneuver Velocity & Load Factor 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 Turn Radius?
In this formula, Turn Radius uses Pull-Up Maneuver Velocity & Load Factor. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Turn Radius = (Pull-Down Maneuver Velocity^2)/([g]*(Load Factor+1))
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