CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE

April 2017
Vol-3, Issue-2
Paper ID: 5053
ISSN: 2395-4396
Downloads: 124
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Abstract & Details

Research Area
Aeronautical Engineering
Keywords
Wedge Supersonic flow Wave angle Wedge-angle Variation Mach number Variation Oblique Shock Detached Shock Computational Fluid Dynamics Ansys-Fluent.
Abstract
A wedge is triangular shaped geometrical structure. It is mostly used as supersonic airfoils and nose of supersonic airplanes. It is typically inclined plane which is at an angle with the horizontal. This paper helps in explaining most of the concepts related to wedge. In this paper the principle of working of wedges with the variation of half-wedge angle and also with variation of Mach number has been done. Theoretical analysis of supersonic flow over wedge is also done. The variation of flow parameters like Pressure, Temperature and Mach number is visualised using computational fluid Dynamics and it’s contours and graphs has been plotted. The simulation of shockwave (attached and detached) through CFD is also analyzed.
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Author Information

# Name Institute / Affiliation
1 Pankaj Kumar Singh Institute of Engineering & Technology, Bhagwant University
2 Amrendra Kumar Tripathi Institute of Engineering & Technology, Bhagwant University
3 Er. Satyendra Kumar Rana Institute of Engineering & Technology, Bhagwant University

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APA Style
Singh, Pankaj Kumar, Tripathi, Amrendra Kumar, & Rana, Er. Satyendra Kumar (2017). CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE. International Journal of Advance Research and Innovative Ideas In Education, 3(2), 5645-5663.
MLA Style
Singh, Pankaj Kumar, et al. "CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE." International Journal of Advance Research and Innovative Ideas In Education, vol. 3, no. 2, 2017, pp. 5645-5663.
IEEE Style
Pankaj Kumar Singh, Amrendra Kumar Tripathi, and Er. Satyendra Kumar Rana, "CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE," International Journal of Advance Research and Innovative Ideas In Education, vol. 3, no. 2, pp. 5645-5663, 2017.
Vancouver Style
Singh Pankaj Kumar, Tripathi Amrendra Kumar, Rana Er. Satyendra Kumar. CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE. International Journal of Advance Research and Innovative Ideas In Education. 2017;3(2):5645-5663.
Harvard Style
Singh, Pankaj Kumar, Tripathi, Amrendra Kumar, & Rana, Er. Satyendra Kumar (2017) 'CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE', International Journal of Advance Research and Innovative Ideas In Education, 3(2), pp. 5645-5663.
Chicago Style
Singh, Pankaj Kumar, Amrendra Kumar Tripathi, and Er. Satyendra Kumar Rana. "CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE." International Journal of Advance Research and Innovative Ideas In Education 3, no. 2 (2017): 5645-5663.
Turabian Style
Singh, Pankaj Kumar, Amrendra Kumar Tripathi, and Er. Satyendra Kumar Rana. "CFD ANALYSIS FOR SUPERSONIC FLOW OVER A WEDGE." International Journal of Advance Research and Innovative Ideas In Education 3, no. 2 (2017): 5645-5663.

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