Effectiveness of Cone Angle on Surface Pressure Distribution along Slant Length of a Cone at Hypersonic Mach Numbers

Authors

  • Javed Shoukat Shaikh Department of Applied Sciences and Humanities, MIT School of Engineering, MITADT University, Pune-412201, Maharashtra, India
  • Khizar Ahmed Pathan Department of Mechanical Engineering, Trinity College of Engineering and Research, Pune, India
  • Krishna Kumar Department of Applied Sciences and Humanities, MIT School of Engineering, MITADT University, Pune-412201, Maharashtra, India
  • Sher Afghan Khan Department of Mechanical Engineering, Faculty of Engineering, IIUM, Gombak Campus, Kuala Lumpur, Malaysia

DOI:

https://doi.org/10.37934/arfmts.104.1.185203

Keywords:

Cone, hypersonic flow, surface pressure

Abstract

In the present study, the prime attention is to numerically simulate the surface pressure distribution over the slant length of the cone at the various Mach numbers and for the considerable range of semi-cone angles. The Computational Fluid Dynamics (CFD) analysis is used to simulate the surface pressure distribution numerically. The hypersonic Mach numbers, semi-cone angle, and various locations along the slant length of a cone are considered parameters for this research work. The Mach numbers (M) considered for the research work are 5, 7, 9, 11, 13, and 15. The cone angle (θ) from 5° to 25° is considered. The results of pressure (P/Pa) are recorded at various locations (x/L) along the slant length of the cone as 0.1 to 1. The pressure distribution results are obtained by CFD analysis and compared with the analytical results available in the literature for Mach number 5. The findings obtained by CFD analysis and analytical results show good agreement. In this investigation, it is observed that the Mach number, cone angle, and slant length of the cone are the highly influential parameters for the surface pressure distribution. The pressure distribution over the slant length of the cone increases with an increase in the Mach number and the semi-cone angle.

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Author Biographies

Javed Shoukat Shaikh, Department of Applied Sciences and Humanities, MIT School of Engineering, MITADT University, Pune-412201, Maharashtra, India

jss21.aero@gmail.com

Khizar Ahmed Pathan, Department of Mechanical Engineering, Trinity College of Engineering and Research, Pune, India

dr.knpathan@gmail.com

Krishna Kumar, Department of Applied Sciences and Humanities, MIT School of Engineering, MITADT University, Pune-412201, Maharashtra, India

krishna.icoer@gmail.com

Sher Afghan Khan, Department of Mechanical Engineering, Faculty of Engineering, IIUM, Gombak Campus, Kuala Lumpur, Malaysia

sakhan@iium.edu.my

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Published

2023-05-02

How to Cite

Javed Shoukat Shaikh, Khizar Ahmed Pathan, Krishna Kumar, & Khan, S. A. (2023). Effectiveness of Cone Angle on Surface Pressure Distribution along Slant Length of a Cone at Hypersonic Mach Numbers. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 104(1), 185–203. https://doi.org/10.37934/arfmts.104.1.185203

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