Author name: Arshad Arif A.S

Nozzle performance analysis calculator

The performance analysis of a nozzle typically involves parameters such as exit velocity, mass flow rate, and efficiency. One common formula used for analyzing nozzle performance is the ideal nozzle equation: Where: Ve​ is the exit velocity of the fluid from the nozzle. g is the acceleration due to gravity. ΔℎΔh is the pressure difference across

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Shock-boundary layer interaction Calculator

The shock-boundary layer interaction is a complex phenomenon in fluid dynamics, particularly in high-speed aerodynamics. There isn’t a single formula to describe it, as it depends on various factors such as flow conditions, geometry, and boundary layer characteristics. However, researchers often use empirical correlations, numerical simulations, or theoretical models to study and predict these interactions.

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