作者其他论文
文献详情
Aerodynamic performance of waverider forebody integrated with inlet and isolator
文献类型:会议
作者:Liu, Zhenxia[1]  Xiao, Hong[2]  Wu, Dingyi[3]  Lian, Xiaochun[4]  
机构:[1]School of Power and Energy, Northwestern Polytechnical University, Shaan'xi, Xi'an, 710072, China
[2]School of Power and Energy, Northwestern Polytechnical University, Shaan'xi, Xi'an, 710072, China
[3]School of Power and Energy, Northwestern Polytechnical University, Shaan'xi, Xi'an, 710072, China
[4]School of Power and Energy, Northwestern Polytechnical University, Shaan'xi, Xi'an, 710072, China
年:2007
通讯作者:Liu, Z.
会议名称:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
页码范围:4009-4015
会议地点:Cincinnati, OH, United states
会议开始日期:2007-07-08
会议结束日期:2007-07-11
收录情况:EI(20075010968253)  
所属部门:动力与能源学院
人气指数:538
浏览次数:531
语言:外文
摘要:
A method for the design of an integrated forebody-inlet-isolator waverider configuration using osculating analysis is presented. Simulation studies were conducted to investigate forebody-inlet-isolator performance in an airframe-scramjet integrated hypersonic vehicle. Inlet unstart characteristics resulted from variations in geometry and flow-field properties are included in simulation studies. Simulation results indicate that the forebody-inlet and isolators are of simple configuration but they ...More
0
评论(0 条评论)
登录