%0 Journal Article
%T Numerical study of the dynamics performance of the supersonic inlet for air-breathing pulse detonation engine<br>脉冲爆震发动机进气道气动性能的数值研究
%A Wang Dingxi
%A Yan Chuanjun
%A <br>王丁喜
%A 严传俊
%J 力学学报
%D 2005
%I 
%X A series of numerical computations have been conducted to characterize the movement of the terminal shock inside an axisymmetric supersonic inlet under three different outlet conditions: sinusoidal perturbation pressure, experimental gauge pressure history at the head wall of a PDE and blocking the outlet of inlet. The relationship between the movement of terminal shock and the outlet conditions is demonstrated. The governing equations are discretized by finite volume method. The inviscid flux at the interfaces of control volumes is calculated using three order upwind interpolation, while the corresponding viscous flux is obtained using two order centered difference scheme. The minmod limiter is introduced to eliminate the non-physical elements of solutions. For steady computation, time-dependent method is used; for unsteady computation, dual time stepping method is used. The discretized algebraic equations are solved using alternate direction iteration method.
%K pulse detonation engine
%K supersonic inlet
%K pressure perturbation
%K terminal shock
%K multi-block structured grid<br>脉冲爆震发动机
%K 超音速进气道
%K 结尾正激波
%K 扰动压力
%K 多块结构化网格
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=4100DA4A1A3BA1B0CE5AD99AE1DFB420&aid=98DA82C9FAA70734&yid=2DD7160C83D0ACED&vid=42425781F0B1C26E&iid=B31275AF3241DB2D&sid=583C993D4E08F5CE&eid=B75DC817262E20A8&journal_id=0459-1879&journal_name=力学学报&referenced_num=1&reference_num=10