Computational Fluid Dynamics and Experimental Validations of the Direct Coupling Between Interior, Intermediate and Exterior Ballistics Using the Euler Equations

Author:

Cayzac Roxan1,Carette Eric2,Alziary de Roquefort Thierry3,Renard François-Xavier4,Roux Dominique4,Balbo Patrick4,Patry Jean-Noël5

Affiliation:

1. Head of Aerodynamics, Technical Direction, Nexter Munitions, 7 Route de Guerry, 18023 Bourges Cedex, France; Associate Professor of the Universities, National School of Engineering at Bourges, 88 Boulevard Lahitolle, 18020 Bourges Cedex

2. Research Associate in Aerodynamics, Technical Direction, Nexter Munitions, 7 Route de Guerry, 18023 Bourges Cedex, France

3. Professor of the University of Poitiers, Expert Consulting in Fluid Mechanics, 129 Rue des Quatres Roues, 86000 Poitiers, France

4. Engineering Department, Nexter Systems, 7 Route de Guerry, 18023 Bourges Cedex, France

5. Product Development Manager, Engineering Department, Nexter Systems 13 Route de la Minière, 78034 Versailles Cedex, France e-mail:

Abstract

For several years we have been working on the development of a computational fluid dynamics ballistics code called FREIN. This code is the result of a strong cooperation between Nexter Munitions and the University of Poitiers. In the last years, efforts have been carried out to improve the 3D modeling. In a fully unsteady way, the interior, intermediate and exterior ballistics were modeled as well as the weapon system environment. The complex phenomena encountered are investigated by an adapted numerical simulation approach using the Euler equations for two immiscible gases. The method involves moving bodies with respect to fixed Cartesian meshes and the aerodynamic forces are used to compute the trajectories. In this paper, theoretical developments and computations have been applied mainly to the simulation of the firing of an advanced 120 mm lightweight tank demonstrator. In comparison with firing experiments, first computation validation results concerning interior ballistics, muzzle brake flow, sabot discard and blast wave propagation and reflection are presented and are very satisfactory.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference32 articles.

1. Computation of Compressible Multifluids;Abgrall;J. Comput. Phys.

2. Solution Adaptative Cartesian Grid Methods for Aerodynamic Flows with Complex Geometries;Aftosmis

3. Local Adaptative Mesh Refinement for Shock Hydrodynamics;Berger;J. Comput. Phys., Elsevier

4. Computation of Sabot Discard Using Chimera Technique;Champigny

5. A Flight Mechanics/Aerodynamics Coupling Methodology for Projectiles;Dietrich

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3