Project Details
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Dynamics of Swirl and Jet Flames (SWJET)

Subject Area Hydraulic and Turbo Engines and Piston Engines
Acoustics
Fluid Mechanics
Technical Thermodynamics
Term from 2020 to 2024
Project identifier Deutsche Forschungsgemeinschaft (DFG) - Project number 441269395
 
Final Report Year 2024

Final Report Abstract

Thermoacoustic instabilities pose significant challenges to developing flexible, reliable, and safe gas turbines, particularly in terms of power range and fuel composition, including hydrogen. Addressing these challenges is essential for creating low-emission gas turbines contributing to carbon-free power generation systems. The SWJET project aims to advance the monolithic understanding of thermoacoustic instabilities in jet and swirl flames. This project is divided into two main components: a numerical approach based on the theory of linearized fields and experimental validation data, in the continuation of a predecessor project. Experimental and simulation results highlight the impact of pilot flames on perfectly and technically premixed flame shapes and their corresponding flame transfer functions. The current numerical project also documents the first application of linearized analysis to turbulent flames, emphasizing the linearization of heat release rate models and the challenges involved. Additionally, special attention is given to the generation and transport of inertial waves and their role in amplification mechanisms.

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Additional Information

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