摘要
根据隐身飞机的设计特点 ,对各种改善进气道隐身性能的技术措施进行了概述。通过对理论计算和试验研究结果的分析 。
Various technical approaches to improved air inlet capability in terms of the low observability of aircraft are presented. The analysis and test investigations of some effective concepts for reduced air inlet RCS were performed.
出处
《飞机设计》
2003年第3期6-9,共4页
Aircraft Design
