Critical Temperature Calculator

Critical temperature  can refer to the temperature associated with a critical condition during aerodynamic analysis, often involving compressible flows. This temperature represents a significant point in the analysis of an aircraft’s performance and behavior, where specific thermodynamic considerations become essential for accurate assessments. The formula to calculate Critical Temperature as follows:

Where:

  • T0 is the stagnation temperature in Kelvin,
  • γ is the Specific heat ratio.

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