期刊名称：International Journal of Advances in Engineering and Management
电子版ISSN：2395-5252
出版年度：2021
卷号：3
期号：11
页码：869-874
DOI：10.35629/5252-0311650654
语种：English
出版社：IJAEM JOURNAL
摘要：Scramjet inlets are an important part of their operation and their design has important implications for overall engine performance. Therefore, the forward-facing position of the engine inlet should be consistent with the body position of the vehicle. These geometric changes have a dramatic effect on the flow of several elements. Air intakes incorporating various ramps that produce oblique shocks followed by cowl shocks are selected to increase the capture of air masses. Disruptive shock may force the boundary layer to separate from the wall, resulting in a total loss of pressure gain and a decrease in the efficiency of the entry. Design an entry point to meet requirements such as lower position pressure, high vertical pressure and gain temperature and flow reduction to the required Mach number. A two dimensional analysis is being done on this project.
