Performance analysis for high-speed missile inlets

被引：3

作者：

Bourdeau, C ^{[1
]}

Blaize, M ^{[1
]}

Knight, D ^{[1
]}

机构：

[1] Rutgers State Univ, Dept Mech & Aerosp Engn, Piscataway, NJ 08854 USA

来源：

JOURNAL OF PROPULSION AND POWER | 2000年 / 16卷 / 06期

关键词：

D O I：

10.2514/2.5687

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A new methodology, Euler semiempirical simulation for three-dimensional inlets (2ES3D), has been developed to predict three-dimensional missile inlet aerodynamic performance within a small fraction of the time required for conventional Reynolds averaged Navier-Stokes solvers, The 2ES3D method is based on an Euler dow solver with a virtual terminal shock model and an analytical subsonic diffuser model. The details and validation of the methodology are presented.

引用

页码：1125 / 1131

页数：7

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