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Performance Analysis of a Pulsejet Engine

By Shashank Ranjan Chaurasia, Rajesh Gupta, R. M. Sarviya and Bhopal (m. P. India


This paper investigates the performance of U-type pulsejet engine whose overall length is approximately 160 cm. Gas dynamics, acoustics and chemical kinetics were modeled to gain an understanding of various physical phenomena affecting pulsejet operation, scalability, and efficiency. The pulsejet was run in valveless mode on LPG fuel. Pressure, temperature, thrust, specific impulse, and concentrations of CO, NO and HC at exit of pulse jet engine were measured. Thrust is found to increase with increasin

Year: 2014
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