Design of Valve Less Pulsejet Engine

Authors

  • Ramkrishan Dutta Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Shivam Vrat Sharma Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Rajat Sharma Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Uttam Kumar Saini Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Vikas Chauhan Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Aman Vyas Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India
  • Sanjay Kumar Palsaniya Student, Department of Mechanical Engineering, Global Institute of Technology, Jaipur, India

Keywords:

pulse jet engine, detonation, valve less, combustion, thrust

Abstract

Pulse detonation engines also known as pulse jet engines are categorization of internal combustion engine that eliminate the key component present in the rest of the jet engine i.e. compressor and turbine. The entire internal combustion engine is less efficient. Having few to almost no moving parts such jet engine could become the next technology in the field of aviation and space technology. Though this technology was first observed in the mid-20th century. Using the geometry as the huge factor for producing thrust through the intake and exhaust pipe, pulse jets rely on the compressibility of intake air and the type of fuel for better combustion efficiency.

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Published

29-07-2021

Issue

Section

Articles

How to Cite

[1]
R. Dutta, “Design of Valve Less Pulsejet Engine”, IJRESM, vol. 4, no. 7, pp. 339–341, Jul. 2021, Accessed: Apr. 23, 2024. [Online]. Available: https://journal.ijresm.com/index.php/ijresm/article/view/1100