Interaction Behavior of Pulsejet Engines

Author:

Maqbool Daanish1,Cadou Christopher P.1

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Abstract

Valveless pulsejet engines are analyzed as electric circuits in which the main engine components (inlet, combustion chamber, and tailpipe) are assigned impedance values and represented using a system of linear equations. The solution to these equations yields Bode plots for the engines that can be used to predict operating frequency as well as the effects of individual component dimensions on overall engine behavior. This method of analysis is found to predict engine operating frequencies to within 7% of experimentally measured values. The analysis is extended to include systems of multiple engines and again verified by comparison to experiment. It is shown that multiple engines can be locked in phase or in antiphase predictably by selecting the proper interconnection method. The latter has important implications for noise reduction and for propulsion applications involving arrays of pulsejets.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference20 articles.

1. LockwoodR. M. “Pulse-Reactor Low Cost Lift-Propulsion Engines,” AIAA Paper 1964-0172, May 1964. 10.2514/6.1964-172

2. CloydJ. R. “Summary Report on Investigation of Miniature Valveless Pulsejets,” U.S. Army Transportation Research Command Rept. 64-20, Feb. 1964.

3. MooreM. D. “Personal Air Vehicles: A Rural/Regional and Intra-Urban On-Demand Transportation System,” AIAA Paper 2003-2646, July 2003. 10.2514/6.2003-2646

4. SkorupaJ. “Military Airlift—Catching the Next Wave,” AIAA Paper 2003-2747, July 2003. 10.2514/6.2003-2747

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