• Shivam Sudarshan Verma
• Abhipsa Dasbabu
• Parikshit Baruah
• Rohit Das
• Anwesha Dasbabu

Jet engine is an energy conversion device. It converts chemical energy into a rotatory mechanical energy. It works on the concept of Brayton Cycle. In this work, a combustion chamber has been designed for a turbocharger-based jet engine. Calculations have been done for the designing of a combustion chamber in the engine. The system has also been modelled in CREO and proper materials have been selected. The system has been designed for sustaining the temperature of 1300 K. LPG is used as a fuel in the system and the demonstration has been carried out without any accidents and promising results have been attained.

"Design and calculations of a combustion chamber for a turbojet engine", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 1, page no.2116-2120, January 2019, Available :http://www.jetir.org/papers/JETIRDY06334.pdf

"Design and calculations of a combustion chamber for a turbojet engine", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 1, page no. pp2116-2120, January 2019, Available at : http://www.jetir.org/papers/JETIRDY06334.pdf