Thrust Angle for Unaccelerated Level Flight for given Drag Calculator

✖Drag Force is the resisting force experienced by an object moving through a fluid.ⓘ Drag Force [F_D]			+10% -10%
✖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 for Unaccelerated Level Flight for given Drag [σ_T]

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Thrust Angle for Unaccelerated Level Flight for given Drag Solution

STEP 0: Pre-Calculation Summary

Formula Used

Thrust Angle = acos(Drag Force/Thrust)
σ_T = acos(F_D/T)
This formula uses 2 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)
acos - The inverse cosine function, is the inverse function of the cosine function. It is the function that takes a ratio as an input and returns the angle whose cosine is equal to that ratio., acos(Number)

Variables Used

Thrust Angle - (Measured in Radian) - Thrust Angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.
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.

STEP 1: Convert Input(s) to Base Unit

Drag Force: 99.99 Newton --> 99.99 Newton No Conversion Required
Thrust: 100 Newton --> 100 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ_T = acos(F_D/T) --> acos(99.99/100)

Evaluating ... ...

σ_T = 0.0141422534775199

STEP 3: Convert Result to Output's Unit

0.0141422534775199 Radian --> No Conversion Required

FINAL ANSWER

0.0141422534775199 ≈ 0.014142 Radian <-- Thrust Angle

(Calculation completed in 00.033 seconds)

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Created by Vinay Mishra

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

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

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< Thrust and Power Requirements Calculators

Thrust Angle for Unaccelerated Level Flight for given Lift

LaTeX Go Thrust Angle = asin((Weight of Body-Lift Force)/Thrust)

Weight of Aircraft in Level, Unaccelerated Flight

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

Thrust for Level and Unaccelerated Flight

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

Thrust Angle for Unaccelerated Level Flight for given Drag

LaTeX Go Thrust Angle = acos(Drag Force/Thrust)

Thrust Angle for Unaccelerated Level Flight for given Drag Formula

LaTeX Go

Thrust Angle = acos(Drag Force/Thrust)
σ_T = acos(F_D/T)

What is Thrust Vectoring?

Thrust vectoring, also known as thrust vector control, is the ability of an aircraft, rocket, or other vehicle to manipulate the direction of the thrust from its engine(s) or motor(s) to control the attitude or angular velocity of the vehicle.

How to Calculate Thrust Angle for Unaccelerated Level Flight for given Drag?

Thrust Angle for Unaccelerated Level Flight for given Drag calculator uses Thrust Angle = acos(Drag Force/Thrust) to calculate the Thrust Angle, Thrust Angle for Unaccelerated Level Flight for given Drag refers to the angle at which the thrust produced by the aircraft's propulsion system is directed relative to the flight path during level flight, where the aircraft's velocity remains constant. Thrust Angle is denoted by σ_T symbol.

How to calculate Thrust Angle for Unaccelerated Level Flight for given Drag using this online calculator? To use this online calculator for Thrust Angle for Unaccelerated Level Flight for given Drag, enter Drag Force (F_D) & Thrust (T) and hit the calculate button. Here is how the Thrust Angle for Unaccelerated Level Flight for given Drag calculation can be explained with given input values -> 0.014142 = acos(99.99/100).

FAQ

What is Thrust Angle for Unaccelerated Level Flight for given Drag?

Thrust Angle for Unaccelerated Level Flight for given Drag refers to the angle at which the thrust produced by the aircraft's propulsion system is directed relative to the flight path during level flight, where the aircraft's velocity remains constant and is represented as σ_T = acos(F_D/T) or Thrust Angle = acos(Drag Force/Thrust). Drag Force is the resisting force experienced by an object moving through a fluid & The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.

How to calculate Thrust Angle for Unaccelerated Level Flight for given Drag?

Thrust Angle for Unaccelerated Level Flight for given Drag refers to the angle at which the thrust produced by the aircraft's propulsion system is directed relative to the flight path during level flight, where the aircraft's velocity remains constant is calculated using Thrust Angle = acos(Drag Force/Thrust). To calculate Thrust Angle for Unaccelerated Level Flight for given Drag, you need Drag Force (F_D) & Thrust (T). With our tool, you need to enter the respective value for Drag Force & Thrust 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 Thrust Angle?

In this formula, Thrust Angle uses Drag Force & Thrust. We can use 1 other way(s) to calculate the same, which is/are as follows -

Thrust Angle = asin((Weight of Body-Lift Force)/Thrust)

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