Computational Study of Flow Through Truncated Plug Nozzle

Authors

  • K. Yashwanth Bharath Student, Department of Aeronautical Engineering, Paavai Engineering College, Namakkal, India
  • J. Praveen Student, Department of Aeronautical Engineering, Paavai Engineering College, Namakkal, India
  • E. Akash Student, Department of Aeronautical Engineering, Paavai Engineering College, Namakkal, India
  • R. Arravind Professor, Department of Aeronautical Engineering, Paavai Engineering College, Namakkal, India

Keywords:

bell shaped rocket nozzle, Aerospike nozzle, second law of thermodynamics

Abstract

Conical plug nozzle and truncated conical plug nozzle are advanced rocket nozzles suitable for use as altitude compensating nozzles. The conical plug and truncated conical plug nozzles are numerically simulated to first validate with experimental data and then to compare with the experimental results.

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Published

26-06-2021

Issue

Vol. 2 No. 6 (2021)

Section

Articles

License

Copyright (c) 2021 K. Yashwanth Bharath, J. Praveen, E. Akash

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
K. Yashwanth Bharath, J. Praveen, E. Akash, and R. Arravind, “Computational Study of Flow Through Truncated Plug Nozzle”, IJRAMT, vol. 2, no. 6, pp. 185–186, Jun. 2021, Accessed: Dec. 22, 2024. [Online]. Available: https://journals.ijramt.com/index.php/ijramt/article/view/900