Drag for Level and Unaccelerated Flight Calculator

✖The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.ⓘ Thrust [T]			+10% -10%
✖Thrust Angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.ⓘ Thrust Angle [σ_T]			+10% -10%

✖Drag Force is the resisting force experienced by an object moving through a fluid.ⓘ Drag for Level and Unaccelerated Flight [F_D]

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Drag for Level and Unaccelerated Flight Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Force = Thrust*cos(Thrust Angle)
F_D = T*cos(σ_T)
This formula uses 1 Functions, 3 Variables

Functions Used

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

Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Thrust - (Measured in Newton) - The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.
Thrust Angle - (Measured in Radian) - Thrust Angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.

STEP 1: Convert Input(s) to Base Unit

Thrust: 100 Newton --> 100 Newton No Conversion Required
Thrust Angle: 0.01 Radian --> 0.01 Radian No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_D = T*cos(σ_T) --> 100*cos(0.01)

Evaluating ... ...

F_D = 99.9950000416665

STEP 3: Convert Result to Output's Unit

99.9950000416665 Newton --> No Conversion Required

FINAL ANSWER

99.9950000416665 ≈ 99.995 Newton <-- Drag Force

(Calculation completed in 00.004 seconds)

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Credits

Created by Vinay Mishra

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

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

Verified by 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 300+ more calculators!

< Lift and Drag Requirements Calculators

Lift for Unaccelerated Flight

LaTeX Go Lift Force = Weight of Body-Thrust*sin(Thrust Angle)

Drag for Level and Unaccelerated Flight at Negligible Thrust Angle

LaTeX Go Drag Force = Dynamic Pressure*Area*Drag Coefficient

Lift for Level and Unaccelerated Flight at Negligible Thrust Angle

LaTeX Go Lift Force = Dynamic Pressure*Area*Lift Coefficient

Drag for Level and Unaccelerated Flight

LaTeX Go Drag Force = Thrust*cos(Thrust Angle)

Drag for Level and Unaccelerated Flight Formula

LaTeX Go

Drag Force = Thrust*cos(Thrust Angle)
F_D = T*cos(σ_T)

How does drag affect airplane flight?

Drag is defined as the force that delays or slows the forward movement of an airplane through the air.

How to Calculate Drag for Level and Unaccelerated Flight?

Drag for Level and Unaccelerated Flight calculator uses Drag Force = Thrust*cos(Thrust Angle) to calculate 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 F_D symbol.

How to calculate Drag for Level and Unaccelerated Flight using this online calculator? To use this online calculator for Drag for Level and Unaccelerated Flight, enter Thrust (T) & Thrust Angle (σ_T) and hit the calculate button. Here is how the Drag for Level and Unaccelerated Flight calculation can be explained with given input values -> 99.995 = 100*cos(0.01).

FAQ

What is Drag for Level and Unaccelerated Flight?

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 and is represented as F_D = T*cos(σ_T) or Drag Force = Thrust*cos(Thrust Angle). The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air & Thrust Angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.

How to calculate Drag for Level and Unaccelerated Flight?

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 is calculated using Drag Force = Thrust*cos(Thrust Angle). To calculate Drag for Level and Unaccelerated Flight, you need Thrust (T) & Thrust Angle (σ_T). With our tool, you need to enter the respective value for Thrust & Thrust 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 Drag Force?

In this formula, Drag Force uses Thrust & Thrust Angle. We can use 2 other way(s) to calculate the same, which is/are as follows -

Drag Force = Dynamic Pressure*Area*Drag Coefficient
Drag Force = Power/Freestream Velocity

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