Specific Temperature at Throat Formula

Fx Copy
LaTeX Copy
Specific Temperature represents the temperature of the gas flowing through the throat per unit mass. Check FAQs
Tt=2T1γ+1
Tt - Specific Temperature?T1 - Temperature at Chamber?γ - Specific Heat Ratio?

Specific Temperature at Throat Example

With values
With units
Only example

Here is how the Specific Temperature at Throat equation looks like with Values.

Here is how the Specific Temperature at Throat equation looks like with Units.

Here is how the Specific Temperature at Throat equation looks like.

219.7425Edit=2256Edit1.33Edit+1
You are here -
HomeIcon Home » Category Physics » Category Aerospace » Category Propulsion » fx Specific Temperature at Throat

Specific Temperature at Throat Solution

Follow our step by step solution on how to calculate Specific Temperature at Throat?

FIRST Step Consider the formula
Tt=2T1γ+1
Next Step Substitute values of Variables
Tt=2256K1.33+1
Next Step Prepare to Evaluate
Tt=22561.33+1
Next Step Evaluate
Tt=219.742489270386K
LAST Step Rounding Answer
Tt=219.7425K

Specific Temperature at Throat Formula Elements

Variables
Specific Temperature
Specific Temperature represents the temperature of the gas flowing through the throat per unit mass.
Symbol: Tt
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Temperature at Chamber
Temperature at Chamber typically refers to the temperature inside a closed chamber or enclosure.
Symbol: T1
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Specific Heat Ratio
The specific heat ratio describes the ratio of specific heats of a gas at constant pressure to that at constant volume.
Symbol: γ
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.

Other formulas in Nozzles category

​Go Propulsion Efficiency
ηprop=2(v0v9)1+(v0v9)2
​Go Specific Volume at Throat
Vt=V1(γ+12)1γ-1
​Go Characteristics Velocity
C=([R]T1γ)(γ+12)γ+1γ-1
​Go Nozzle Thrust Coefficient
CF=FAtP1

How to Evaluate Specific Temperature at Throat?

Specific Temperature at Throat evaluator uses Specific Temperature = (2*Temperature at Chamber)/(Specific Heat Ratio+1) to evaluate the Specific Temperature, Specific Temperature at Throat represents the temperature at the throat of the nozzle.this equation provides a simple relationship between the temperature at the nozzle inlet and the temperature at the throat of the nozzle, taking into account the specific heat ratio of the gas. Specific Temperature is denoted by Tt symbol.

How to evaluate Specific Temperature at Throat using this online evaluator? To use this online evaluator for Specific Temperature at Throat, enter Temperature at Chamber (T1) & Specific Heat Ratio (γ) and hit the calculate button.

FAQs on Specific Temperature at Throat

What is the formula to find Specific Temperature at Throat?
The formula of Specific Temperature at Throat is expressed as Specific Temperature = (2*Temperature at Chamber)/(Specific Heat Ratio+1). Here is an example- 219.7425 = (2*256)/(1.33+1).
How to calculate Specific Temperature at Throat?
With Temperature at Chamber (T1) & Specific Heat Ratio (γ) we can find Specific Temperature at Throat using the formula - Specific Temperature = (2*Temperature at Chamber)/(Specific Heat Ratio+1).
Can the Specific Temperature at Throat be negative?
No, the Specific Temperature at Throat, measured in Temperature cannot be negative.
Which unit is used to measure Specific Temperature at Throat?
Specific Temperature at Throat is usually measured using the Kelvin[K] for Temperature. Celsius[K], Fahrenheit[K], Rankine[K] are the few other units in which Specific Temperature at Throat can be measured.
Copied!