Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Air Resistance Force
Air Resistance=Air Constant*Velocity^2 GO
Archimedes Principle
Archimedes Principle=Density*Acceleration Due To Gravity*Velocity GO
Wavelength Of The Wave(Using Velocity)
Wavelength Of A Wave=Velocity*Time Period Of Progressive Wave GO
Time Period (Using Velocity )
Time Period Of Progressive Wave=Wavelength/Velocity GO
Stokes Force
Stokes Force=6*pi*Radius*Dynamic viscosity*Velocity GO
Angular Frequency (Using Velocity )
Angular Frequency=(2*pi*Velocity)/Wavelength GO
Centripetal Force
Centripetal Force=(Mass*(Velocity)^2)/Radius GO
Frequency Of Wavelength ( Using Velocity )
frequency=Velocity/Wavelength Of A Wave GO
Wave Number (Using Angular Frequency)
Wave Number=Angular Frequency/Velocity GO
Kinetic Energy
Kinetic Energy=(Mass*Velocity^2)/2 GO
Wavelength Of The Wave(Using Frequency)
Wavelength=Velocity/frequency GO

5 Other formulas that calculate the same Output

Turn rate for a given lift coefficient
Turn Rate=[g]*(sqrt((Reference Area*Freestream density*lift coefficient*Load factor)/(2*Weight))) GO
Turn rate for a given wing loading
Turn Rate=[g]*(sqrt(Freestream density*lift coefficient*Load factor/(2*Wing Loading))) GO
Turn rate
Turn Rate=[g]*(sqrt((Load factor^2)-1))/Velocity GO
Pull-down maneuver rate
Turn Rate=[g]*(1+Load factor)/Velocity GO
Turn rate for a high load factor
Turn Rate=[g]*Load factor/Velocity GO

Pull-up maneuver rate Formula

Turn Rate=[g]*(Load factor-1)/Velocity
ω=[g]*(n-1)/v
More formulas
Pull-up maneuver radius GO
Velocity for a given pull-up maneuver radius GO
Load factor for a given pull-up maneuver radius GO
Load factor for a given pull-up maneuver rate GO
Velocity for a given pull-up maneuver rate GO
Pull-down maneuver radius GO
Velocity for a given pull-down maneuver radius GO
Load factor for a given pull-down maneuver radius GO
Pull-down maneuver rate GO
Velocity for a given pull-down maneuver rate GO
Load factor for a given pull-down maneuver rate GO

What are aerobatic maneuvers?

Aerobatic maneuvers are flight paths putting aircraft in unusual attitudes, in air shows, dogfights, or competition aerobatics.

How to Calculate Pull-up maneuver rate?

Pull-up maneuver rate calculator uses Turn Rate=[g]*(Load factor-1)/Velocity to calculate the Turn Rate, The Pull-up maneuver rate for an aircraft depends upon the load factor and velocity of the aircraft. Turn Rate and is denoted by ω symbol.

How to calculate Pull-up maneuver rate using this online calculator? To use this online calculator for Pull-up maneuver rate, enter Load factor (n) and Velocity (v) and hit the calculate button. Here is how the Pull-up maneuver rate calculation can be explained with given input values -> 1.872932 = [g]*(1.2-1)/60.

FAQ

What is Pull-up maneuver rate?
The Pull-up maneuver rate for an aircraft depends upon the load factor and velocity of the aircraft and is represented as ω=[g]*(n-1)/v or Turn Rate=[g]*(Load factor-1)/Velocity. Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft and Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). .
How to calculate Pull-up maneuver rate?
The Pull-up maneuver rate for an aircraft depends upon the load factor and velocity of the aircraft is calculated using Turn Rate=[g]*(Load factor-1)/Velocity. To calculate Pull-up maneuver rate, you need Load factor (n) and Velocity (v). With our tool, you need to enter the respective value for Load factor and Velocity 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 Rate?
In this formula, Turn Rate uses Load factor and Velocity. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Turn Rate=[g]*(sqrt((Load factor^2)-1))/Velocity
  • Turn Rate=[g]*(1+Load factor)/Velocity
  • Turn Rate=[g]*Load factor/Velocity
  • Turn Rate=[g]*(sqrt((Reference Area*Freestream density*lift coefficient*Load factor)/(2*Weight)))
  • Turn Rate=[g]*(sqrt(Freestream density*lift coefficient*Load factor/(2*Wing Loading)))
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