This tool predicts the properties of a supersonic flow undergoing an isentropic expansion around a convex corner. It utilizes a mathematical function, derived from fluid dynamics principles, to relate the Mach number, flow deflection angle, and other crucial parameters like pressure and temperature. For example, given the initial Mach number and the angle of the corner, the tool can calculate the resulting Mach number and other flow properties downstream of the expansion.
Accurate prediction of supersonic expansion properties is essential in the design of high-speed aircraft, rocket nozzles, and other supersonic flow systems. This analytical method offers a quick and efficient way to estimate these properties, reducing the reliance on computationally intensive methods like Computational Fluid Dynamics (CFD) in preliminary design stages. Its development marked a significant advancement in the understanding of supersonic flow phenomena.
