Title: Numerical simulation of the form and development of rocket gas near flow field
Abstract: The complicated wave system exists around the near region of the solid rocket motor. The interaction between expansion and compressed wave is the important part of correlated study on plane-missile and missile-warship. The distribution of the pressure and temperature field of complicated wave system is the direct factor which causes the dynamical and hot impact. It is difficult to study the complicated properties of jet flow field by means of experimental method. A method of numerical analysis was applied to study the wave system existing in near rocket gas field and the initial shock wave of high-unexpanded gas jet flow. The properties of the near region of gas flow field have obtained from the numerical result. The data accord with those given in reference and provide helpful information.
Publication Year: 2003
Publication Date: 2003-01-01
Language: en
Type: article
Access and Citation
Cited By Count: 2
AI Researcher Chatbot
Get quick answers to your questions about the article from our AI researcher chatbot