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.

1.
Dowling
,
A. P.
, 1996, “
Acoustics of Unstable Flows
,” in
Theoretical and Applied Mechanics
,
T.
Tatsumi
,
E.
Watanabe
, and
T.
Kambe
, eds.,
Elsevier
, Amsterdam, pp.
171
186
.
2.
Marble
,
F. E.
, and
Candel
,
S. M.
, 1977, “
Acoustic Disturbances From Gas Non-uniformities Convected Through a Nozzle
,”
J. Sound Vib.
0022-460X,
55
(
2
), pp.
225
243
.
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.
Muthukrishnan
,
M.
,
Strahle
,
W. C.
, and
Neale
,
D. H.
, 1978, “
Separation of Hydrodynamic, Entropy, and Combustion Noise in a Gas Turbine Combustor
,”
AIAA J.
0001-1452,
16
(
4
), pp.
320
327
.
5.
Sattelmayer
,
T.
, 2000, “
Influence of the Combustor Aerodynamics on Combustion Instabilities From Equivalence Ratio Fluctuations
,” ASME Paper No. 2000-GT-0082.
6.
Polifke
,
W.
,
Paschereit
,
C. O.
, and
Döbbeling
,
K.
, 2001, “
Constructive and Destructive Interference of Acoustic and Entropy Waves in a Premixed Combustor With a Choked Exit
,”
Int. J. Acoust. Vib.
1027-5851,
6
(
3
), pp.
135
146
.
7.
Eckstein
,
J.
,
Freitag
,
E.
,
Hirsch
,
C.
, and
Sattelmayer
,
T.
, 2004, “
Experimental Study on the Role of Entropy Waves in Low-Frequency Oscillations for a Diffusion Burner
,” ASME Paper No. GT2004-54163.
8.
Eckstein
,
J.
, 2004, “
On the Mechanisms of Combustion Driven Low-Frequency Oscillations in Aero-engines
,” dissertation, Technische Universität München, München, Germany.
9.
Shenoda
,
F. B.
, 1973, “
Reflexionsarme Abschlüsse für durchströmte Kanäle
,” dissertation, Technische Universität Berlin.
10.
Forster
,
S. F.
,
Roehle
,
I.
, and
Michel
,
U.
, 2004, “
Optimierung der passiven und aktiven Dämpfung von thermoakustischen Schwingungen
,” Abschlussbericht 4.4.2C, Deutsches Zentrum für Luft-und Raumfahrt, DLR, Berlin Charlottenburg. AG Turbo II-Verbundprojekt für ein CO2-armes Kraftwerk.
11.
Maier
,
R.
,
Zillmann
,
J.
,
Roure
,
A.
,
Winninger
,
M.
,
Enghardt
,
L.
,
Tapken
,
U.
,
Neise
,
W.
,
Antoine
,
H.
, and
Bouty
,
E.
, 2001, “
Active Control of Fan Tone Noise From Aircraft Engines
,” 7th AIAA/CEAS Aeroacoustics Conference, Paper No. 2001-2220.
12.
Enghardt
,
L.
,
Zhang
,
Y.
, and
Neise
,
W.
, 1999, “
Experimental Verification of a Radial Mode Analysis Technique Using Wall-Flush Mounted Sensors
,”
J. Acoust. Soc. Am.
0001-4966,
105
, p.
1186
.
13.
Flemming
,
F.
,
Olbricht
,
C.
,
Wegner
,
B.
,
Sadiki
,
A.
,
Janicka
,
J.
,
Bake
,
F.
,
Michel
,
U.
,
Lehmann
,
B.
, and
Röhle
,
I.
, 2005, “
Analysis of Unsteady Motion with Respect to Noise Sources in a Gas Turbine Combustor: Isothermal Flow Case
,”
Flow, Turbul. Combust.
1386-6184,
75
(
1–4
), pp.
3
27
.
14.
Duan
,
X. R.
,
Weigand
,
P.
,
Meier
,
W.
,
Keck
,
O.
,
Stricker
,
W.
,
Aigner
,
M.
, and
Lehmann
,
B.
, 2004, “
Experimental Investigations and Laser Based Validation Measurements in a Gas Turbine Model Combustor
,”
Prog. Comput. Fluid Dyn.
1468-4349,
4
, pp.
175
182
.
15.
Duan
,
X. R.
,
Meier
,
W.
,
Weigand
,
P.
, and
Lehmann
,
B.
, 2005, “
Phase-Resolved Laser Raman Scattering and Laser Doppler Velocimetry Applied to Periodic Instabilities in a Gas Turbine Model Combustor
,”
Appl. Phys. B
0946-2171,
80
, pp.
389
396
.
You do not currently have access to this content.