Computational Analysis of Aerodynamic Parameters For Supersonic Artillery Projectiles

International Journal of Mechanical Engineering
© 2020 by SSRG - IJME Journal
Volume 7 Issue 8
Year of Publication : 2020
Authors : Md Rafiqur Rahman
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How to Cite?

Md Rafiqur Rahman, "Computational Analysis of Aerodynamic Parameters For Supersonic Artillery Projectiles," SSRG International Journal of Mechanical Engineering, vol. 7,  no. 8, pp. 5-17, 2020. Crossref, https://doi.org/10.14445/23488360/IJME-V7I8P102

Abstract:

Aerodynamic parameters have a huge impact on a projectile trajectory, which in turn results in its range and accuracy. The influence aerodynamic parameters for the estimation of trajectory elements are drag Coefficients, lift Coefficients, attack angles, muzzle velocity, atmospheric conditions, and the projectile shape and size. Thus proper methods for determining the drag and lift forces of the projectile is very important. The trajectory of a projectile through the air is affected both by gravity and by aerodynamic forces. In this paper, 57 mm and 37 mm anti-aircraft projectile was considered for the AnalysisAnalysis. Her main emphasis was given to determine the pressure coefficient, Drag coefficients, lift coefficient of the projectiles at different attack angles. The experiment was conducted in an open circuit subsonic wind tunnel to study the aerodynamic parameters where the uniform flow velocity is maintained across the flow direction. For the investigation, varied angles of the attack were considered. Here inclined manometer was used to determine the static surface pressure, and the pressure coefficient was determined from that. Then the drag & lift forces and their coefficients were determined. Finally, for the computational AnalysisAnalysis, the ANSYS Software was used to simulate the experimental data.

Keywords:

Aerodynamic Parameters, Projectile, Drag Force, Lift Force, Pressure Coefficient, Drag Coefficient, Lift Coefficient, Angle of Attack, Computational Analysis, Ansys software

References:

[1] Mohammad A. D. and Slobodan J, Various Methods of Artillery Projectiles Base Drag Reduction, 8th International Scientific Conference on defence Technology Belgrade, Serbia, (2018).
[2] Chand K. K. and Pattnaik S, Modeling Projectile Motion: A System Dynamics Approach, International Journal on Information Science and Computing Orissa India, 2(1) (2008).
[3] Goran. J. O, Bosko P. R, and Aleksandar C. B, Aerodynamic Shape Optimization of Guided Missile Based on Wind Tunnel Testing and Computational Fluid Dynamics Simulation, Serbia, Scientific Paper, 21(3) (2017) (1543-1554).
[4] Sahoo S. and Laha M.K, Coefficient of Drag and Trajectory Simulation of 130 mm Supersonic Artillery Shell with Recovery Plug of Fuze, Defence Science Journal, India, 64 (6) (2014 ) (502-508).
[5] Jian S, Shaobo F, Yaxin J, Zhu Q, and Duan J, Aerodynamics Analysis of a Hypersonic Electromagnetic Gun Launched Projectile, Journal Pre-Proof China, Ref. DT, 592 ( 2020).
[6] Mahfouz E. W, Zhengui H, and Zhihua C, Aerodynamic Characteristics and Flow Field Investigations of an Optimal Hollow Projectile, 5th International Conference on Mechanical Engineering and Mechanics China, (2014).
[7] A.Anish, Suthen.P.G, Viju.M.K, Modelling and Analysis of a Car for Reducing Aerodynamic Forces, International Journal of Engineering Trends and Technology, V47(1) (2017) 1-17. ISSN:2231-5381. www.ijettjournal.org. published by seventh sense research group.
[8] Damir DJ and Marija S,The Aerodynamic Characteristics Determination of Classic Symmetric Projectile, 5thInternational Symposium about forming and design in Mechanical Engineering Serbia, (2008).
[9] Kiran and Basawaraj, Drag Prediction and validation of Standard M549, 155mm Projectile, International Journal of Engineering Research and Reviews India, 2(3) (2014) (26-32).
[10] Suliman M. A, Mahmoud O. K, Al Sanabawy M. A, and Abdel Hamid O.E, Computational Investigation of Base Drag Reduction for a Projectile at Different Flight Regimes, 13th International Conference on Aerospace Science and Aviation technology Coiro Egypt, (2009).
[11] Ruth PriyankaPonnala, Dr.B.Subbaratnam, Design and dynamic analysis of a fuze body Outer case used in a guided missile, SSRG International Journal of Mechanical Engineering 1(6) (2014) 11-15.
[12] Elsaadany A. and Wenjun YI, “Investigation on Trajectory Correction for Typical Artillery Projectiles” 5th International Conference on Mechanical Engineering and Mechanics China, (2014).
[13] Alexey. ML, Stanislav, A.K, Ivan. GR, Optimization of Aerodynamic Form of Projectiles for Solving the Problem of Shooting Range Increasing, AIP Conference Proceeding 1893, (2017) 030085.
[14] Shabnam J, Nekkanti S, and Sriram K, Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap, International Journal of Rotating Machinery, India,(2015).