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Flight Speed refers to the velocity at which an aircraft moves through the air. Check FAQs
V=Ve-Tidealma
V - Flight Speed?Ve - Exit Velocity?Tideal - Ideal Thrust?ma - Mass Flow Rate?

Flight Speed given Ideal Thrust Example

With values
With units
Only example

Here is how the Flight Speed given Ideal Thrust equation looks like with Values.

Here is how the Flight Speed given Ideal Thrust equation looks like with Units.

Here is how the Flight Speed given Ideal Thrust equation looks like.

111Edit=248Edit-479.5Edit3.5Edit
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Flight Speed given Ideal Thrust Solution

Follow our step by step solution on how to calculate Flight Speed given Ideal Thrust?

FIRST Step Consider the formula
V=Ve-Tidealma
Next Step Substitute values of Variables
V=248m/s-479.5N3.5kg/s
Next Step Prepare to Evaluate
V=248-479.53.5
LAST Step Evaluate
V=111m/s

Flight Speed given Ideal Thrust Formula Elements

Variables
Flight Speed
Flight Speed refers to the velocity at which an aircraft moves through the air.
Symbol: V
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Exit Velocity
Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine.
Symbol: Ve
Measurement: SpeedUnit: m/s
Note: Value can be positive or negative.
Ideal Thrust
Ideal Thrust is the thrust produced by an engine when nozzle exit pressure is same as ambient pressure or nozzle is perfectly expanded.
Symbol: Tideal
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Mass Flow Rate
Mass Flow Rate represents the amount of mass passing through a system per unit of time.
Symbol: ma
Measurement: Mass Flow RateUnit: kg/s
Note: Value should be greater than 0.

Other Formulas to find Flight Speed

​Go Flight Speed given Momentum of Ambient Air
V=Mma
​Go Flight Speed given Ram Drag and Mass Flow Rate
V=Dramma

Other formulas in Thrust Generation category

​Go Total Thrust given Efficiency and Enthalpy
Ttotal=ma((2Δhnozzleηnozzle)-V+(ηTηtransmissionΔhturbine))
​Go Ideal Thrust given Effective Speed Ratio
Tideal=maV((1α)-1)
​Go Thrust power
TP=maV(Ve-V)
​Go Specific thrust
Isp=Ve-V

How to Evaluate Flight Speed given Ideal Thrust?

Flight Speed given Ideal Thrust evaluator uses Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate to evaluate the Flight Speed, Flight Speed given Ideal Thrust is a measure of an aircraft's forward velocity, calculated by considering the ideal thrust, the exit velocity and the mass flow rate, providing a crucial parameter for aircraft performance evaluation and optimization. Flight Speed is denoted by V symbol.

How to evaluate Flight Speed given Ideal Thrust using this online evaluator? To use this online evaluator for Flight Speed given Ideal Thrust, enter Exit Velocity (Ve), Ideal Thrust (Tideal) & Mass Flow Rate (ma) and hit the calculate button.

FAQs on Flight Speed given Ideal Thrust

What is the formula to find Flight Speed given Ideal Thrust?
The formula of Flight Speed given Ideal Thrust is expressed as Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate. Here is an example- 118.5714 = 248-479.5/3.5.
How to calculate Flight Speed given Ideal Thrust?
With Exit Velocity (Ve), Ideal Thrust (Tideal) & Mass Flow Rate (ma) we can find Flight Speed given Ideal Thrust using the formula - Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate.
What are the other ways to Calculate Flight Speed?
Here are the different ways to Calculate Flight Speed-
  • Flight Speed=Momentum of Ambient Air/Mass Flow RateOpenImg
  • Flight Speed=Ram Drag/Mass Flow RateOpenImg
Can the Flight Speed given Ideal Thrust be negative?
No, the Flight Speed given Ideal Thrust, measured in Speed cannot be negative.
Which unit is used to measure Flight Speed given Ideal Thrust?
Flight Speed given Ideal Thrust is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Flight Speed given Ideal Thrust can be measured.
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