%0 Journal Article
%T Research on waverider configuration method<br>乘波飞行器构型方法研究
%A Wang Famin Li Liwei Yao Wenxiu Lei Maifang Laboratory of High Temperature Gas Dynamics
%A Institute of Mechanics
%A Chinese Academy of Sciences
%A Beijing
%A China
%A <br>王发民
%A 李立伟
%A 姚文秀
%A 雷麦芳
%J 力学学报
%D 2004
%I 
%X In hypersonic flow, as the increase of Mach number, the wave drag and friction drag also enlarge, and this will form a hysonic L/D "barrier". But waverider can efficiently overcome this "barrier". In this paper we develop a wedge-elliptical cone waverider configuration method, study on front body-scramjet engine integration design, and create a hypersonic waverider. In terms of numerical result and wind test data, it is different from traditional waveriders that this waverider can offer not only high L/D ratio, but also the uniform flow field with high temperature and high press which is requireed by scramjet engine.
%K waverider
%K wedge-elliptical cone waverider
%K aerodynamic
%K lift-drag ratio<br>乘波飞行器
%K 变楔角楔/椭圆锥乘波体
%K 气动力
%K 升阻比
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=4100DA4A1A3BA1B0CE5AD99AE1DFB420&aid=3AEF84D7C22FE724&yid=D0E58B75BFD8E51C&vid=933658645952ED9F&iid=94C357A881DFC066&sid=F9A6B6F259CE5121&eid=89389F643CA3F778&journal_id=0459-1879&journal_name=力学学报&referenced_num=7&reference_num=8