• Bahadur Singh Mohne
• Prakash Pandey

Pulsejet engines are considered a feasible option for the propulsion of missiles and rockets owing to their advantageous characteristics of reduced weight and superior performance. The primary objective of this research is to use computational fluid dynamics (CFD) in order to evaluate the thermal properties and thrust generation of a pulsejet propulsion system. The ANSYS CFX software is used for conducting computational fluid dynamics (CFD) simulations of pulsejet engines. The analysis of the impact of multiple fuel inlets is conducted by a computational fluid dynamics (CFD) research, employing an eddy dissipation combustion model. The computational fluid dynamics (CFD) research demonstrates that an augmentation in fuel inlets results in a proportional elevation in outlet pressure and thrust force

Pulsejet, Fuel Inlet, Combustion, CFD, Thrust

"Thermal Analysis of Pulsejet Combustion using CFX", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.10, Issue 9, page no.g395-g398, September 2023, Available :http://www.jetir.org/papers/JETIR2309660.pdf

"Thermal Analysis of Pulsejet Combustion using CFX", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.10, Issue 9, page no. ppg395-g398, September 2023, Available at : http://www.jetir.org/papers/JETIR2309660.pdf