TIME-ACCURATE COMPUTATIONAL FLUID-DYNAMICS APPROACH TO TRANSONIC STORE SEPARATION TRAJECTORY PREDICTION

被引:64
作者
LIJEWSKI, LE
SUHS, NE
机构
[1] Wright Laboratory, Eglin Air Force Base, Florida
[2] Calspan Corporation, Arnold Air Force Base, Tennessee
[3] Weapon Airframe Research Section, Flight Vehicles Branch, Weapon Flight Mechanics Division
来源
JOURNAL OF AIRCRAFT | 1994年 / 31卷 / 04期
关键词
Computational fluid dynamics - Euler flow - Grid methodology - Time accurate store separation - Transonic store separation trajectory;
D O I
10.2514/3.46575
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A computational fluid dynamic technique is demonstrated for a time-accurate store separation event at transonic speeds. An overlapping grid approach is used coupled with an implicit Euler flow solver with a flux-difference split scheme based on Roe's approximate Riemann solver and a six-degree-of-freedom trajectory code. All major trends of the trajectory are captured and surface pressure distributions are predicted. Three sources of error are identified and discussed.
引用
收藏
页码:886 / 891
页数:6
相关论文
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