TY - CHAP A1 - Geyer, Thomas A1 - Moreau, Danielle J. A1 - Sarradj, Ennes A1 - Doolan, Con T1 - Zur Schallentstehung an dreidimensionalen wandgebundenen Tragflügelprofilen T2 - Fortschritte der Akustik - DAGA 2018, 44. Jahrestagung für Akustik, 19.-22. März 2018 in München Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/geyer_wandgebundeneprofile_daga2018.pdf SP - 1587 EP - 1590 PB - Deutsche Gesellschaft für Akustik CY - Berlin ER - TY - CHAP A1 - Sharma, Sparsh A1 - Sarradj, Ennes A1 - Schmidt, Heiko T1 - Low-Fidelity Stochastic Approach for Airfoil-Turbulence Interaction Noise T2 - Fortschritte der Akustik - DAGA 2018, 44. Jahrestagung für Akustik, 19.-22. März 2018 in München Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/sharma_stochastic_daga2018.pdf SP - 1184 EP - 1187 PB - Deutsche Gesellschaft für Akustik CY - Berlin ER - TY - CHAP A1 - Henke, Anna-Sophia A1 - Noack, Martin A1 - Sarradj, Ennes T1 - Untersuchung des Modalverhaltens strukturierter Bleche T2 - Fortschritte der Akustik - DAGA 2018, 44. Jahrestagung für Akustik, 19.-22. März 2018 in München Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/henke_modalverhalten_daga2018.pdf SP - 469 EP - 472 PB - Deutsche Gesellschaft für Akustik CY - Berlin ER - TY - GEN A1 - Kisler, Roman A1 - Sarradj, Ennes T1 - Plate Silencers for Broadband Low Frequency Sound Attenuation T2 - Acta Acustica united with Acustica N2 - An efficiency improvement for the implementation of a semi-analytical model of plate silencers in ducts is presented in this work. It is shown that a high approximation quality can be maintained even if the computation effort is reduced significantly. Thus, preliminary designs of plate silencers for specific purposes can be conducted with little effort. In addition, the accelerated implementation is utilized to perform an extensive parameter variation in order to find a best case configuration of silen properties and corresponding design rules. The results of these studies show that a tuning of plate and geometry parameters allow for substantial increases in a silencer's attenuation performance. Y1 - 2018 SN - 1610-1928 SN - 1861-9959 VL - 104 IS - 3 SP - 521 EP - 527 ER - TY - GEN A1 - Moreau, Danielle J. A1 - Geyer, Thomas A1 - Doolan, Con A1 - Sarradj, Ennes T1 - Surface curvature effects on the tonal noise of a wall-mounted finite airfoil T2 - The Journal of the Acoustical Society of America N2 - This paper is concerned with the influence of camber on the noise of a wall-mounted finite airfoil with natural boundary layer transition. Tonal noise measurements taken in an aeroacoustic wind tunnel are presented for airfoils with aspect ratio of 2, NACAxx12 profile and camber between 0 and 6% at 40% chord. The results show camber is an important parameter that determines the operating conditions for which acoustic tone generation occurs and the number and intensity of the tones produced. Airfoils with 0%–2% camber have an acoustic signature that is dominated by a high amplitude primary tone, whereas the spectra of airfoils with higher camber of 4%–6% feature a more pronounced side tone structure. Tonal noise production does not collapse with lift coefficient, demonstrating that the local flow conditions influence the noise source. Tonal noise production is explained in terms of changes to mean flow topology, namely the location of flow separation, which is linked to tonal noise generation. Scaling of airfoil tonal noise is found to vary with angle of attack and pressure gradient. Empirical scaling laws for the primary tone frequency dependence on velocity are also derived for the cambered airfoils. Y1 - 2018 U6 - https://doi.org/10.1121/1.5040981 SN - 1520-8524 VL - 143 IS - 6 SP - 3460 EP - 3473 ER - TY - GEN A1 - Geyer, Thomas A1 - Moreau, Danielle J. A1 - Giesler, Jens A1 - Hall, Philipp A1 - Sarradj, Ennes A1 - Doolan, Con T1 - Measurement of the noise generated by wall-mounted airfoils of different thickness T2 - 24th AIAA/CEAS Aeroacoustics Conference 2018, Atlanta, USA, 25 June - 29 June 2018, (AIAA 2018-3796) Y1 - 2018 UR - https://arc.aiaa.org/doi/abs/10.2514/6.2018-3796 SN - 978-1-62410-560-9 PB - AIAA CY - Reston, Va ER - TY - GEN A1 - Geyer, Thomas A1 - Sharma, Sparsh A1 - Sarradj, Ennes T1 - Detached Eddy Simulation of the Flow Noise Generation of Cylinders with Porous Cover T2 - 24th AIAA/CEAS Aeroacoustics Conference 2018, Atlanta, USA, 25 June - 29 June 2018, (AIAA 2018-3472) Y1 - 2018 UR - https://arc.aiaa.org/doi/abs/10.2514/6.2018-3472 SN - 978-1-62410-560-9 PB - AIAA CY - Reston, Va ER - TY - GEN A1 - Çaldichoury, Iñaki A1 - Souli, Mhamed A1 - Sarradj, Ennes A1 - Geyer, Thomas A1 - Del Pin, Facundo T1 - Numerical investigation of flow around hairy flaps cylinder using FSI Capabilities T2 - The International journal of multiphysics Y1 - 2018 SN - 2048-3961 SN - 1750-9548 VL - 12 IS - 2 SP - 189 EP - 208 ER - TY - CHAP A1 - Sharma, Sparsh A1 - Sarradj, Ennes T1 - Fluctuating inflow conditions for time-domain boundary element method for airfoil-turbulence interaction noise T2 - Proceedings of the 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines ISUAAAT15, 24-27 September 2018, University of Oxford, UK Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/sharma_turbulence_ISUAAAT2018.pdf PB - ISUAAAT Scientific Committee ER - TY - CHAP A1 - Geyer, Thomas A1 - Sarradj, Ennes T1 - Noise reduction and aerodynamics of airfoils with porous trailing edges T2 - INTER-NOISE 2018, the 47th International Congress and Exposition on Noise Control Engineering, Chicago, Illinois, USA Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/geyer_porousTE_internoise2018.pdf ER - TY - CHAP A1 - Sharma, Sparsh A1 - Geyer, Thomas A1 - Sarradj, Ennes T1 - Time Domain Boundary Element Method for the Leading-Edge Noise subjected to Linear Vorticity T2 - INTER-NOISE 2018, the 47th International Congress and Exposition on Noise Control Engineering, Chicago, Illinois, USA Y1 - 2018 UR - https://www-docs.b-tu.de/fg-akustik/public/veroeffentlichungen/sharma_bem_internoise2018.pdf ER - TY - GEN A1 - Geyer, Thomas A1 - Lucius, Andreas A1 - Schrödter, Marcus A1 - Schneider, Marc A1 - Sarradj, Ennes T1 - Reduction of Turbulence Interaction Noise Through Airfoils With Perforated Leading Edges T2 - Acta Acustica united with Acustica Y1 - 2019 U6 - https://doi.org/10.3813/AAA.919292 SN - 1610-1928 SN - 1436-7947 VL - 105 IS - 1 SP - 109 EP - 122 ER - TY - GEN A1 - Geyer, Thomas A1 - Kamps, Laura A1 - Sarradj, Ennes A1 - Brücker, Christoph T1 - Vortex Shedding and Modal Behavior of a Circular Cylinder Equipped with Flexible Flaps T2 - Acta Acustica united with Acustica Y1 - 2019 U6 - https://doi.org/10.3813/aaa.919301 SN - 1610-1928 SN - 1436-7947 VL - 105 IS - 1 SP - 210 EP - 219 ER -