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[PDF][PDF] Modeling combustion chamber acoustics using the DLR TAU code

T Horchler, W Armbruster, J Hardi, S Karl… - researchgate.net
This paper investigates the numerical properties of the DLR TAU code as a tool for
combustion instability research. Starting from simple ideal gas test cases of closed cavities …
被引用次数：6 相关文章

Modeling combustion chamber acoustics using the DLR TAU code

T Horchler, W Armbruster, J Hardi, S Karl… - Space Propulsion …, 2018 - elib.dlr.de
This paper investigates the numerical properties of the DLR TAU code as a tool for
combustion instability research. Starting from simple ideal gas test cases of closed cavities …

Modeling Combustion Chamber Acoustics Using the DLR TAU Code

T Horchler, S Karl, K Hannemann, A Gernoth… - Space Propulsion …, 2018 - elib.dlr.de
Combustion chamber instabilities are poorly understood and remain a major concern during
the design phase of rocket thrust chambers. It is therefore desirable to develop numerical …