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Excitation of aircraft cabin noise by tightly integrated propulsion systems (C05)

Subject Area Fluid Mechanics
Term since 2023
Project identifier Deutsche Forschungsgemeinschaft (DFG) - Project number 498601949
 
The project predicts the acoustic fuselage surface pressure fluctuations, generated by a complex, thrust vectoring propulsor. Configurations with podded and tightly integrated engines will be considered. Further-more, the acoustic relevance of morphing techniques regarding nozzle and rear fuselage deformation is investigated. These pressure data are coupled via an interface to a structural code to analyze the cabin excitation. To capture all source mechanisms the highly efficient Tam & Auriault source model concept is generalized, to enable accelerations by installation and thrust vectoring, and interaction of the convecting pressure near field with surfaces. This extended approach will be validated by zonal LES simulation.
DFG Programme CRC/Transregios
Applicant Institution Technische Universität Braunschweig
 
 

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