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Drag Force is the resisting force experienced by an object moving through a fluid. Check FAQs
FD=Tcos(σT)
FD - Drag Force?T - Thrust?σT - Thrust Angle?

Drag for Level and Unaccelerated Flight Example

With values
With units
Only example

Here is how the Drag for Level and Unaccelerated Flight equation looks like with Values.

Here is how the Drag for Level and Unaccelerated Flight equation looks like with Units.

Here is how the Drag for Level and Unaccelerated Flight equation looks like.

99.995Edit=100Editcos(0.01Edit)
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Drag for Level and Unaccelerated Flight Solution

Follow our step by step solution on how to calculate Drag for Level and Unaccelerated Flight?

FIRST Step Consider the formula
FD=Tcos(σT)
Next Step Substitute values of Variables
FD=100Ncos(0.01rad)
Next Step Prepare to Evaluate
FD=100cos(0.01)
Next Step Evaluate
FD=99.9950000416665N
LAST Step Rounding Answer
FD=99.995N

Drag for Level and Unaccelerated Flight Formula Elements

Variables
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
The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.
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 can be positive or negative.
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 Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
FD=PdynamicACD
​Go Total Drag Force given required Power
FD=PV

Other formulas in Lift and Drag Requirements category

​Go Lift for Unaccelerated Flight
FL=Wbody-Tsin(σT)
​Go Lift for Level and Unaccelerated Flight at Negligible Thrust Angle
FL=PdynamicACL
​Go Coefficient of Drag for given Thrust-to-Weight Ratio
CD=CLTW
​Go Coefficient of Lift for given Thrust-to-Weight Ratio
CL=CDTW

How to Evaluate Drag for Level and Unaccelerated Flight?

Drag for Level and Unaccelerated Flight evaluator uses Drag Force = Thrust*cos(Thrust Angle) to evaluate the Drag Force, The Drag for Level and Unaccelerated Flight seems to imply a relationship between the drag force and the thrust of an aircraft at a certain thrust angle, the aircraft's thrust from its engines must overcome this drag to maintain a constant velocity. Drag Force is denoted by FD symbol.

How to evaluate Drag for Level and Unaccelerated Flight using this online evaluator? To use this online evaluator for Drag for Level and Unaccelerated Flight, enter Thrust (T) & Thrust Angle T) and hit the calculate button.

FAQs on Drag for Level and Unaccelerated Flight

What is the formula to find Drag for Level and Unaccelerated Flight?
The formula of Drag for Level and Unaccelerated Flight is expressed as Drag Force = Thrust*cos(Thrust Angle). Here is an example- 99.995 = 100*cos(0.01).
How to calculate Drag for Level and Unaccelerated Flight?
With Thrust (T) & Thrust Angle T) we can find Drag for Level and Unaccelerated Flight using the formula - Drag Force = Thrust*cos(Thrust Angle). This formula also uses Cosine function(s).
What are the other ways to Calculate Drag Force?
Here are the different ways to Calculate Drag Force-
  • Drag Force=Dynamic Pressure*Area*Drag CoefficientOpenImg
  • Drag Force=Power/Freestream VelocityOpenImg
Can the Drag for Level and Unaccelerated Flight be negative?
No, the Drag for Level and Unaccelerated Flight, measured in Force cannot be negative.
Which unit is used to measure Drag for Level and Unaccelerated Flight?
Drag for Level and Unaccelerated Flight is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Drag for Level and Unaccelerated Flight can be measured.
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