A Review: Drag Reduction in Aerospace Vehicles Using Aerospikes

Authors

  • Vishnu Kashyap Amity Institute of Aerospace Engineering, Amity University, Uttar Pradesh, India
  • Navdeep Singh Amity Institute of Aerospace Engineering, Amity University, Uttar Pradesh, India
  • Shivani Sharma Amity Institute of Aerospace Engineering, Amity University, Uttar Pradesh, India
  • Jayanta Sinha Amity Institute of Aerospace Engineering, Amity University, Uttar Pradesh, India

DOI:

https://doi.org/10.37591/.v8i2.148

Abstract

Vehicles flying in supersonic and hypersonic region develop a bow shock in front of the blunt body leading to an increase in the pressure and temperature. This increased pressure further leads to higher drag and heat transfer depending on the inflow Mach no. A spike at the tip alters the flow field in the vicinity of main body, thereby reducing drag. Our study focuses on how the flow over the main body changes when the spike is attached at the tip, the complete process of drag reduction by the spike and the different factors that are taken in consideration while choosing the spike geometry.


Keywords: Aerospace vehicles, aerospikes, drag reduction

Cite this Article

Vishnu Kashyap, Navdeep Singh, Jayanta Sinha et al. A Review: Drag Reduction in Aerospace Vehicles using Aerospikes. Journal of Aerospace Engineering & Technology. 2018; 8(2): 51–57p.

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Published

2018-10-06

Issue

Vol. 8 No. 2 (2018)

Section

Articles