Inhalt des Dokuments
Publikationen
2001 | |
Konferenzartikel: | |
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53. |
On the use of Helmholtz resonators for damping acoustic pulsations in industrial gas turbines
ASME Turbo Expo, June 4-6, 2001, New Orleans, Louisiana, USA
2001
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52. |
Prediction of combustion oscillations in gas turbine combustors
39th AIAA Aerospace Science Meeting and Exhibit, January 8-11, 2001, Reno, Nevada, USA, AIAA paper no. 2001-484
2001
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51. |
Thermoacoustic simulation of lean premixed flames using an enhanced time-lag model
31st AIAA Fluid Dynamics Conference (Aeroacoustics Section), June 11-14, 2001, Anaheim, California, USA, AIAA paper no. 2001-2794
2001
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50. |
Using CFD for time-delay modeling of premix flames
ASME Turbo Expo, June 4-6, 2001, New Orleans, Louisiana
2001
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2000 | |
Begutachtete Artikel: | |
49. |
Excitation of thermoacoustic instabilities by the interaction of acoustics and unstable swirling flow
AIAA Journal,
38:1025-1034
2000
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Konferenzartikel: | |
48. |
Active combustion control in land-based gas-turbine engines
Topic Oriented Meeting "Intelligent Combustion Control" of the International Flame Research Foundation, September 25-27, 2000, Paris, France
2000
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47. |
Fluid dynamic instabilities in a swirl stabilized burner and their effect on heat release fluctuations
Ziada, Staubli, Flow Induced Vibrations, Balkema
2000
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46. |
Identification and control of unstable modes in an isothermal and reacting swirling jet
In Proceedings of the 8th European Turbulence Conference, Barcelona, Spain 27-30 June 2000, Seite 101-104.
, Editor,Advances in Turbulence, Band VIIIaus
2000
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45. |
Investigation of thermoacoustic oscillations in combustion systems using an acoustic network model
EUROTHERM Seminar No. 67, July 5-7, 2000, Univ of Twente, Enschede, The Netherlandsaus Acoustics of combustion
2000
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44. |
Mode analysis and control in a nonreacting and reacting swirling jet
Bulletin of the American Physical Society / Division of Fluid Dynamics, Annual Meeting, November 19-21, 2000, Washington, DC, USA
2000
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43. |
Numerical and experimental analysis of acoustically excited combustion instabilities in gas turbines
6th AIAA/CEAS Aeroacoustics Conference, June 12-14, 2000, Maui, Hawaii
2000
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42. |
Performance enhancement of gas-turbine combustor by active control of fuel injection and mixing process - theory and practice
Applied vehicle technology panel symposium on active control technology for enhanced performance operation capabilities of military aircraft, land vehicles and sea vehicles, North Atlantic Treaty, May 8-11, 2000, Braunschweig, Germany
2000
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