Minnzinoo

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M Thuri

N L Tun

Zhenlei Li

Northeastern University

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Northeastern University

Beihang University

Xi'an Jiaotong University

Universidad del Noreste

Northeast Forestry University

Beijing University of Technology

Soochow University

Laboratoire de Génie Électrique de Grenoble

Dalian Institute of Chemical Physics

University of Chinese Academy of Sciences

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Aerodynamic Coefficients Prediction for 122 mm Rocket by Using Computational Fluid Dynamics

IOP Conference Series Materials Science and Engineering (2020)

N L Tun M Thuri Minnzinoo Zhenlei Li

Abstract In this study, the Computational Fluid Dynamics code in SolidWorks was used to predict the aerodynamic coefficients of 122 mm rocket in order to get more accurate aerodynamic coefficients and derivatives for flight simulation. This paper presented the governing equations of fluid dynamics applied in SolidWorks and developed the computational model of the rocket. The results were compared against calculated data from an empirical method. The conducted analyses showed that the comparison results are nearly the same. However, the empirical method provided a faster way to obtain results.

Rocket (weapon)

Dynamics

10.1088/1757-899x/816/1/012010

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Citations (6)