Abstract
Screech combustion instabilities continue to be one of the most detrimental and, in fact, fatal issues for the development of a high-performance afterburner. It is essential to study the underlying flow-physics related to the crucial thermo-acoustic coupling to acquire a predictive capability and to evolve a methodology for the attenuation of screech. A versatile test facility using a single V-gutter flame holder was used to generate the predetermined screech frequency of 2000 Hz in a controlled and sustained manner. The test facility had the capability to run the afterburner model under simulated inlet conditions of pressure and temperatures. The critical zone of flame stabilization near the V-gutter flame holder had complete optical access with quartz glass windows to study the vortex shedding phenomena during the afterburner operation. The critical operating parameters of the test rig were measured using a high-speed NI-based data acquisition system. Flow visualization studies using a high-speed shadowgraph technique was effectively used to understand the onset of screech. A FASTCAM SA-4 Photron high-speed camera was used in this experimental investigation. It was found that the cause for the onset of screech was the vortex shedding frequency from the flame holder locking on to the duct transverse acoustic resonant mode frequency.
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Acknowledgments
The authors thank the Director, Gas Turbine Research Establishment, DRDO for sponsoring this project under the Gas Turbine Enabling Technology (GATET) scheme. The authors thank the Director, NAL and the Head, Propulsion Division for granting permission to take up this project.
Thanks are also due to Sr.Technical Officers Ms Rajeswari Natarajan and Mr A R Jeyaseelan, of the Propulsion Division, CSIR-NAL for their support in the instrumentation work. They would also like to thank Mr Fakruddin Goususab Agadi, Technician-1, Propulsion Division for his technical support. Thanks are also due to Mr J Bimal Patel and Mr K Mukesh ME Students, Dept. of Aerospace Engg. PARK College of Engineering & Technology, Coimbatore and Mr P Srinath, ME Student, Jain University, Department of Aerospace Engineering, Bangalore for their technical support in this project. They would also like to thank project trainees Ms S Madhushree and Mr V Bhuvan Prathap for their technical support and Mr S Prabhakar, Technician for his help during the experimentation.
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Rajashekar, C. et al. (2021). High-Speed Shadowgraph Flow Visualization Studies on the Mechanism of the Onset of Screech and Its Attenuation in a Model Afterburner Test Rig. In: Mistry, C., Kumar, S., Raghunandan, B., Sivaramakrishna, G. (eds) Proceedings of the National Aerospace Propulsion Conference . Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-5039-3_22
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DOI: https://doi.org/10.1007/978-981-15-5039-3_22
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