Temperature at point one on the airfoil () typically refers to the local temperature of the air or fluid at a specific point on an airfoil’s surface or in its vicinity. Airfoil is the cross-sectional shape of an aircraft wing, and during aerodynamic analysis, various parameters like pressure, velocity, and temperature are measured at different points on the airfoil to understand its performance and behavior. represents the temperature at a specific reference point on or near the airfoil.
- Temperature at point one (T1) in K
- Freestream temperature (T∞) in K
- Pressure at point one (p1) in N/m^2
- Freestream pressure (p∞) in N/m^2
- Specific heat ratio (γ)