Velocity in Accelerated Flight Solution

STEP 0: Pre-Calculation Summary
Formula Used
Velocity = (Radius of Curvature/Mass of Aircraft*(Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle)))^(1/2)
v = (Rcurvature/m*(FL+T*sin(σT)-m*[g]*cos(γ)))^(1/2)
This formula uses 1 Constants, 2 Functions, 7 Variables
Constants Used
[g] - Gravitational acceleration on Earth Value Taken As 9.80665
Functions Used
sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)
cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)
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.
Radius of Curvature - (Measured in Meter) - The Radius of Curvature refers to the radius of the curved path an aircraft follows while climbing.
Mass of Aircraft - (Measured in Kilogram) - Mass of Aircraft is the total mass of the plane at any phase of its mission.
Lift Force - (Measured in Newton) - The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.
Thrust - (Measured in Newton) - Thrust denotes the force exerted by the engine to propel an aircraft forward.
Thrust Angle - (Measured in Radian) - Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.
Flight Path Angle - (Measured in Radian) - Flight Path Angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending.
STEP 1: Convert Input(s) to Base Unit
Radius of Curvature: 2600 Meter --> 2600 Meter No Conversion Required
Mass of Aircraft: 20 Kilogram --> 20 Kilogram No Conversion Required
Lift Force: 200 Newton --> 200 Newton No Conversion Required
Thrust: 700 Newton --> 700 Newton No Conversion Required
Thrust Angle: 0.034 Radian --> 0.034 Radian No Conversion Required
Flight Path Angle: 0.062 Radian --> 0.062 Radian No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
v = (Rcurvature/m*(FL+T*sin(σT)-m*[g]*cos(γ)))^(1/2) --> (2600/20*(200+700*sin(0.034)-20*[g]*cos(0.062)))^(1/2)
Evaluating ... ...
v = 60.3746968438799
STEP 3: Convert Result to Output's Unit
60.3746968438799 Meter per Second --> No Conversion Required
FINAL ANSWER
60.3746968438799 60.3747 Meter per Second <-- Velocity
(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
Vinay Mishra has created this Calculator and 300+ more calculators!
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Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

Climbing Flight Calculators

Flight path angle at given rate of climb
​ LaTeX ​ Go Flight Path Angle = asin(Rate of Climb/Velocity)
Velocity of aircraft at given rate of climb
​ LaTeX ​ Go Velocity = Rate of Climb/sin(Flight Path Angle)
Rate of Climb
​ LaTeX ​ Go Rate of Climb = Velocity*sin(Flight Path Angle)
Weight of Aircraft for given Excess Power
​ LaTeX ​ Go Aircraft Weight = Excess Power/Rate of Climb

Velocity in Accelerated Flight Formula

​LaTeX ​Go
Velocity = (Radius of Curvature/Mass of Aircraft*(Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle)))^(1/2)
v = (Rcurvature/m*(FL+T*sin(σT)-m*[g]*cos(γ)))^(1/2)

What is the acceleration of a plane taking off?

An average commercial jet accelerates to between 120 and 140 knots prior to liftoff. To do this in 30 to 35 seconds requires a good sustained acceleration. This is something that pilots look for during a takeoff roll.

How to Calculate Velocity in Accelerated Flight?

Velocity in Accelerated Flight calculator uses Velocity = (Radius of Curvature/Mass of Aircraft*(Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle)))^(1/2) to calculate the Velocity, The Velocity in Accelerated Flight refers to the speed of the aircraft as it undergoes changes in speed or direction to achieve specific flight objectives, it is typically measured as the airspeed of the aircraft, which is the speed of the aircraft relative to the surrounding air. Velocity is denoted by v symbol.

How to calculate Velocity in Accelerated Flight using this online calculator? To use this online calculator for Velocity in Accelerated Flight, enter Radius of Curvature (Rcurvature), Mass of Aircraft (m), Lift Force (FL), Thrust (T), Thrust Angle T) & Flight Path Angle (γ) and hit the calculate button. Here is how the Velocity in Accelerated Flight calculation can be explained with given input values -> 4.585787 = (radius_of_curvature_eom/20*(200+700*sin(0.034)-20*[g]*cos(0.062)))^(1/2).

FAQ

What is Velocity in Accelerated Flight?
The Velocity in Accelerated Flight refers to the speed of the aircraft as it undergoes changes in speed or direction to achieve specific flight objectives, it is typically measured as the airspeed of the aircraft, which is the speed of the aircraft relative to the surrounding air and is represented as v = (Rcurvature/m*(FL+T*sin(σT)-m*[g]*cos(γ)))^(1/2) or Velocity = (Radius of Curvature/Mass of Aircraft*(Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle)))^(1/2). The Radius of Curvature refers to the radius of the curved path an aircraft follows while climbing, Mass of Aircraft is the total mass of the plane at any phase of its mission, The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow, Thrust denotes the force exerted by the engine to propel an aircraft forward, Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction & 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 in Accelerated Flight?
The Velocity in Accelerated Flight refers to the speed of the aircraft as it undergoes changes in speed or direction to achieve specific flight objectives, it is typically measured as the airspeed of the aircraft, which is the speed of the aircraft relative to the surrounding air is calculated using Velocity = (Radius of Curvature/Mass of Aircraft*(Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle)))^(1/2). To calculate Velocity in Accelerated Flight, you need Radius of Curvature (Rcurvature), Mass of Aircraft (m), Lift Force (FL), Thrust (T), Thrust Angle T) & Flight Path Angle (γ). With our tool, you need to enter the respective value for Radius of Curvature, Mass of Aircraft, Lift Force, Thrust, Thrust Angle & 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 Radius of Curvature, Mass of Aircraft, Lift Force, Thrust, Thrust Angle & Flight Path Angle. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Velocity = Rate of Climb/sin(Flight Path Angle)
  • Velocity = Excess Power/(Thrust-Drag Force)
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