Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : November 07, 2019 - November 08, 2019
The supersonic jet is used on engineering devices and is one of the fundamental problems of the compressible fluid dynamics, and causes the various problems of the aeronautical and other engineering, such as: the design of a rocket: launcher system. It seems that the characteristic of supersonic jets is necessary to control the engineering devices, but the effect of nozzle diameter does not conducted in past papers. This paper aims to clarify the effect of nozzle diameter for characteristic of supersonic jets by the numerical analysis.
