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Drag Force is the resisting force experienced by an object moving through a fluid. Check FAQs
FD=Tcos(σT)-m[g]sin(γ)-ma
FD - Drag Force?T - Thrust?σT - Thrust Angle?m - Mass of Aircraft?γ - Flight Path Angle?a - Acceleration?[g] - Gravitational acceleration on Earth?

Drag in Accelerated Flight Example

With values
With units
Only example

Here is how the Drag in Accelerated Flight equation looks like with Values.

Here is how the Drag in Accelerated Flight equation looks like with Units.

Here is how the Drag in Accelerated Flight equation looks like.

80.043Edit=700Editcos(0.034Edit)-20Edit9.8066sin(0.062Edit)-20Edit30.37Edit
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Drag in Accelerated Flight Solution

Follow our step by step solution on how to calculate Drag in Accelerated Flight?

FIRST Step Consider the formula
FD=Tcos(σT)-m[g]sin(γ)-ma
Next Step Substitute values of Variables
FD=700Ncos(0.034rad)-20kg[g]sin(0.062rad)-20kg30.37m/s²
Next Step Substitute values of Constants
FD=700Ncos(0.034rad)-20kg9.8066m/s²sin(0.062rad)-20kg30.37m/s²
Next Step Prepare to Evaluate
FD=700cos(0.034)-209.8066sin(0.062)-2030.37
Next Step Evaluate
FD=80.0429821420068N
LAST Step Rounding Answer
FD=80.043N

Drag in Accelerated Flight Formula Elements

Variables
Constants
Functions
Drag Force
Drag Force is the resisting force experienced by an object moving through a fluid.
Symbol: FD
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Thrust
Thrust denotes the force exerted by the engine to propel an aircraft forward.
Symbol: T
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Thrust Angle
Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.
Symbol: σT
Measurement: AngleUnit: rad
Note: Value should be greater than 0.
Mass of Aircraft
Mass of Aircraft is the total mass of the plane at any phase of its mission.
Symbol: m
Measurement: WeightUnit: kg
Note: Value should be greater than 0.
Flight Path Angle
Flight Path Angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending.
Symbol: γ
Measurement: AngleUnit: rad
Note: Value should be greater than 0.
Acceleration
Acceleration is the rate of change in velocity to the change in time.
Symbol: a
Measurement: AccelerationUnit: m/s²
Note: Value should be greater than 0.
Gravitational acceleration on Earth
Gravitational acceleration on Earth means that the velocity of an object in free fall will increase by 9.8 m/s2 every second.
Symbol: [g]
Value: 9.80665 m/s²
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.
Syntax: sin(Angle)
cos
Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.
Syntax: cos(Angle)

Other Formulas to find Drag Force

​Go Total Drag for given Excess Power
FD=T-(Pexcessv)

Other formulas in Climbing Flight category

​Go Rate of Climb
RC=vsin(γ)
​Go Flight path angle at given rate of climb
γ=asin(RCv)
​Go Velocity of aircraft at given rate of climb
v=RCsin(γ)
​Go Weight of Aircraft for given Excess Power
W=PexcessRC

How to Evaluate Drag in Accelerated Flight?

Drag in Accelerated Flight evaluator uses Drag Force = Thrust*cos(Thrust Angle)-Mass of Aircraft*[g]*sin(Flight Path Angle)-Mass of Aircraft*Acceleration to evaluate the Drag Force, The Drag in Accelerated Flight refers to the aerodynamic force that opposes the motion of an aircraft as it moves through the air, it acts in the direction opposite to the aircraft's velocity vector, this equation appears to calculate the total drag force during climb flight by considering the thrust from the engines, the weight component opposing the flight path, and any additional acceleration experienced by the aircraft. Drag Force is denoted by FD symbol.

How to evaluate Drag in Accelerated Flight using this online evaluator? To use this online evaluator for Drag in Accelerated Flight, enter Thrust (T), Thrust Angle T), Mass of Aircraft (m), Flight Path Angle (γ) & Acceleration (a) and hit the calculate button.

FAQs on Drag in Accelerated Flight

What is the formula to find Drag in Accelerated Flight?
The formula of Drag in Accelerated Flight is expressed as Drag Force = Thrust*cos(Thrust Angle)-Mass of Aircraft*[g]*sin(Flight Path Angle)-Mass of Aircraft*Acceleration. Here is an example- 80.04298 = 700*cos(0.034)-20*[g]*sin(0.062)-20*30.37.
How to calculate Drag in Accelerated Flight?
With Thrust (T), Thrust Angle T), Mass of Aircraft (m), Flight Path Angle (γ) & Acceleration (a) we can find Drag in Accelerated Flight using the formula - Drag Force = Thrust*cos(Thrust Angle)-Mass of Aircraft*[g]*sin(Flight Path Angle)-Mass of Aircraft*Acceleration. This formula also uses Gravitational acceleration on Earth constant(s) and , Sine (sin), Cosine (cos) function(s).
What are the other ways to Calculate Drag Force?
Here are the different ways to Calculate Drag Force-
  • Drag Force=Thrust-(Excess Power/Velocity)OpenImg
Can the Drag in Accelerated Flight be negative?
No, the Drag in Accelerated Flight, measured in Force cannot be negative.
Which unit is used to measure Drag in Accelerated Flight?
Drag in Accelerated Flight is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Drag in Accelerated Flight can be measured.
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