Asymmetrical Vortex over Slender Body A Computational Approach

Author:

Karn P. K.ORCID,Kumar P.ORCID,Das SudipORCID

Abstract

Computational investigations were carried out on an ogive-cylinder configuration having a slenderness ratio of 7.5. The geometry of the nose tip was generated based on the physical geometry of the nose tip observed under a scanning electron microscope. Time-dependent simulations were performed on the slender body at a diameter Reynolds number of 3.0×104. Results indicated that the onset of vortex asymmetry was mainly due to the micro-tip imperfection existing at the tip. It was also observed that the variation in the roll angle of the model affected the flow physics largely which has been experimentally observed by several researchers in the past. The computed results were in better agreement with the referenced experimental data.

Publisher

Defence Scientific Information and Documentation Centre

Subject

Electrical and Electronic Engineering,Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Biomedical Engineering,General Chemical Engineering

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. STABILITY OF VORTEX SYMMETRY AT FLOW SEPARATION FROM SLENDER BODIES AND CONTROL BY LOCAL GAS HEATING;Vortex Dynamics - Theoretical, Experimental and Numerical Approaches [Working Title];2024-07-16

2. Influence of Roughness on the Asymmetric Flow Field of a Slender Body;International Journal of Aerospace Engineering;2022-07-27

3. Numerical modeling of unsteady subsonic flow over the conical shape body;Journal of Physics: Conference Series;2022-07-01

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