Aerodynamic Characteristics of Unguided Artillery Projectile-Reference-Cited by-同舟云学术

Aerodynamic Characteristics of Unguided Artillery Projectile

Published:2014-07-28 Issue: Volume:1014 Page:165-168
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

Wessam Mahfouz Elnaggar¹,Chen Zhi Hua¹

Affiliation:

1. Nanjing University of Science and Technology

Abstract

The paper presents results of investigation of a flow over unguided artillery projectile in order to understand variation of flow parameters past a 155 mm artillery projectile M107 and the performance of the computational code. Furthermore; static aerodynamic coefficients were calculated. The flow around projectile was solved as 3-D unsteady compressible flow.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.1014.165.pdf

Reference3 articles.

1. Sahu, J., 1991. Transonic Navier-Stokes computations for a spinning body of revolution. Tech. Rep. ARL-TR-3265, U.S. Army Research Laboratory.

2. Weinacht, P., 2003. Prediction of projectile performance, stability, and free-flight motion usingcomputational fluid dynamics. Tech. Rep. ARL-TR-3015, Army Research Laboratory.

3. Robert L. McCoy, Modern Exterior Ballistics, 4thedition, ISBN-0-7643-0720-7, Schiffir Publishing Ltd., (1998).

Cited by 3 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

1. Inverse Reinforcement Learning-Based Fire-Control Command Calculation of an Unmanned Autonomous Helicopter Using Swarm Intelligence Demonstration;Aerospace;2023-03-20

2. The Effect of Surface Roughness on the Trajectory of Howitzer Shell;Journal of the Korea Institute of Military Science and Technology;2022-08-05

3. Effects of spin rate on the surface pressure distribution of a rotating model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-05-07