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.