Velocity of aircraft at a given rate of climb Calculator

Category	Physics ↺
Physics	Flight Stability and Control ↺
Flight-Stability-And-Control	Airplane Performance ↺
Airplane-Performance	Rate of Climb ↺

✖The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time.ⓘ Rate of Climb [R/C]			+10% -10%
✖Flight path angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descendingⓘ Flight path angle [θ]			+10% -10%

✖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). ⓘ Velocity of aircraft at a given rate of climb [v]

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Velocity of aircraft at a given rate of climb

Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad

Sai Venkata Phanindra Chary Arendra has verified this Calculator and 100+ more calculators!

< 9 Other formulas that you can solve using the same Inputs

Velocity in an accelerated flight

Velocity=((Radius of Curvature/Mass)*(Lift force+(Thrust force*sin(Thrust angle))-(Mass*[g]*cos(Flight path angle))))^(1/2) GO

Lift in an accelerated flight

Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)) GO

Thrust in an accelerated flight

Thrust of an aircraft=(sec(Thrust angle))*(Drag Force+(Mass*[g]*sin(Flight path angle))+(Mass*Acceleration)) GO

Drag in an accelerated flight

Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) GO

Centrifugal Force in an accelerated flight

Centrifugal force=Lift force+(Thrust force*sin(Thrust angle))-(Mass*[g]*cos(Flight path angle)) GO

Flight path angle at a given rate of climb

Flight path angle=asin(Rate of Climb/Velocity) GO

Rate of Climb

Rate of Climb=Velocity*sin(Flight path angle) GO

Weight of aircraft for given excess power

Weight=Excess Power/Rate of Climb GO

Excess power for given rate of climb

Excess Power=Rate of Climb*Weight GO

< 11 Other formulas that calculate the same Output

Velocity of the follower after time t (Cycloidal motion)

Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke)))) GO

Velocity of the follower for tangent cam with roller follower(contact with straight flanks)

Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2)) GO

Velocity OF A Progressive Wave

Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave GO

Velocity Of The Particle

Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi) GO

Velocity due to voltage

Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e]) GO

Velocity Of Wave in String

Velocity=sqrt(Tension Of String/Mass Per Unit length) GO

Velocity OF A Progressive Wave(Using Angular Frequency)

Velocity=(Wavelength*Angular Frequency)/(4*pi) GO

Velocity OF A Progressive Wave(Using Frequency)

Velocity=Wavelength Of A Wave*frequency GO

Velocity Of A Wave(Using Wave Number)

Velocity=Angular Frequency/Wave Number GO

Velocity Of Sound In Liquid

Velocity=sqrt(bulk modulus/Density) GO

Velocity Of Sound In Solids

Velocity=sqrt(Elasticity/Density) GO

Velocity of aircraft at a given rate of climb Formula

Velocity=Rate of Climb/sin(Flight path angle)
v=R/C/sin(θ)

More formulas

Rate of Climb GO

Flight path angle at a given rate of climb GO

Excess power GO

Thrust available for given excess power GO

Total Drag for given excess power GO

Velocity of aircraft for given excess power GO

Rate of Climb for given excess power GO

Excess power for given rate of climb GO

Weight of aircraft for given excess power GO

What is a zoom climb?

A zoom climb is a climb where the rate of climb is greater than the maximum climb rate using only the thrust of the aircraft's engines.

How to Calculate Velocity of aircraft at a given rate of climb?

Velocity of aircraft at a given rate of climb calculator uses Velocity=Rate of Climb/sin(Flight path angle) to calculate the Velocity, The Velocity of aircraft at a given rate of climb is given by the ratio of the rate of climb and sine of flight path angle of aircraft. Velocity and is denoted by v symbol.

How to calculate Velocity of aircraft at a given rate of climb using this online calculator? To use this online calculator for Velocity of aircraft at a given rate of climb, enter Rate of Climb (R/C) and Flight path angle (θ) and hit the calculate button. Here is how the Velocity of aircraft at a given rate of climb calculation can be explained with given input values -> 142.8863 = 5/sin(0.035).

FAQ

What is Velocity of aircraft at a given rate of climb?

The Velocity of aircraft at a given rate of climb is given by the ratio of the rate of climb and sine of flight path angle of aircraft and is represented as v=R/C/sin(θ) or Velocity=Rate of Climb/sin(Flight path angle). The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time and Flight path angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending.

How to calculate Velocity of aircraft at a given rate of climb?

The Velocity of aircraft at a given rate of climb is given by the ratio of the rate of climb and sine of flight path angle of aircraft is calculated using Velocity=Rate of Climb/sin(Flight path angle). To calculate Velocity of aircraft at a given rate of climb, you need Rate of Climb (R/C) and Flight path angle (θ). With our tool, you need to enter the respective value for Rate of Climb and Flight path angle 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 Rate of Climb and Flight path angle. We can use 11 other way(s) to calculate the same, which is/are as follows -

Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave
Velocity=Wavelength Of A Wave*frequency
Velocity=(Wavelength*Angular Frequency)/(4*pi)
Velocity=Angular Frequency/Wave Number
Velocity=sqrt(Tension Of String/Mass Per Unit length)
Velocity=sqrt(bulk modulus/Density)
Velocity=sqrt(Elasticity/Density)
Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e])
Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi)
Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke))))
Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2))

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