Method of Characteristics for Design of a Gradual Expansion Supersonic Wind Tunnel Nozzle
The design of a nozzle contour for a supersonic nozzle is a difficult problem, and this article presents a simplified solution for two dimensional supersonic nozzle design. There are two main types of supersonic nozzles. First is a minimum length nozzle, designed for rocket engines. These nozzles achieve isentropic expansion...
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