Investigation of Entropy Noise in Aero-Engine Combustors

Author:

Bake Friedrich1,Michel Ulf1,Roehle Ingo1

Affiliation:

1. Department of Engine Acoustics, Institute of Propulsion Technology, German Aerospace Center (DLR), Mueller-Breslau-Str. 8, 10623 Berlin, Germany

Abstract

Strong evidence is presented that entropy noise is the major source of external noise in aero-engine combustion. Entropy noise is generated in the outlet nozzles of combustors. Low-frequency entropy noise, which was predicted earlier in theory and numerical simulations, was successfully detected in a generic aero-engine combustion chamber. It is shown that entropy noise dominates even in the case of thermo-acoustic resonances. In addition to this, a different noise generating mechanism was discovered that is presumably of even higher relevance to jet engines: There is strong evidence of broad band entropy noise at higher frequencies (1 to 3kHz in the reported tests). This unexpected effect can be explained by the interaction of small scale entropy perturbations (hot spots) with the strong pressure gradient in the outlet nozzle. The direct combustion noise of the flame zone seems to be of minor importance for the noise emission to the ambiance. The combustion experiments were supplemented by experiments with electrical heating. Two different methods for generating entropy waves were used, a pulse excitation and a sinusoidal excitation. In addition, high-frequency entropy noise was generated by steady electrical heating.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference15 articles.

1. Acoustics of Unstable Flows;Dowling

2. Acoustic Disturbances From Gas Non-uniformities Convected Through a Nozzle;Marble;J. Sound Vib.

3. Bohn, M. S. , 1976, “Noise Produced by the Interaction of Acoustic Waves and Entropy Waves With High-Speed Nozzle Flows,” Ph.D. thesis, California Institute of Technology, Pasadena, CA.

4. Separation of Hydrodynamic, Entropy, and Combustion Noise in a Gas Turbine Combustor;Muthukrishnan;AIAA J.

5. Sattelmayer, T. , 2000, “Influence of the Combustor Aerodynamics on Combustion Instabilities From Equivalence Ratio Fluctuations,” ASME Paper No. 2000-GT-0082.

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