2016
DOI: 10.17341/gummfd.34239
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Zamana Bağli Sikiştirilamaz Kavi̇te Akişinin Aeroakusti̇k Anali̇zi̇

Abstract: Kavite akışına ait Rossiter modları incelenmiş ve FW-H Akustik Analoji sonuçları ile karşılaştırılmıştır  FW-H denklemleri geçişli iç yüzey ile 3 boyutlu kavite için incelenmiştir  Türbülansın kavite gürültüsüne etkisi gösterilmiştir

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Cited by 2 publications
(10 citation statements)
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“…U is the incoming free stream velocity magnitude and Ma is the Mach number of the free stream. Phase delay of two vortices separating at the leading wall of cavity is symbolized by α. κ is defined as ratio of vortex convective speed to free stream velocity magnitude [8]. To indicate the details of the eddies past the cavity, the flow field is visualized with isosurfaces past the cavity as shown in Figure 11.…”
Section: Aeroacoustics Results For the Base Flowmentioning
confidence: 99%
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“…U is the incoming free stream velocity magnitude and Ma is the Mach number of the free stream. Phase delay of two vortices separating at the leading wall of cavity is symbolized by α. κ is defined as ratio of vortex convective speed to free stream velocity magnitude [8]. To indicate the details of the eddies past the cavity, the flow field is visualized with isosurfaces past the cavity as shown in Figure 11.…”
Section: Aeroacoustics Results For the Base Flowmentioning
confidence: 99%
“…Additionally, a different permeable acoustic source surface which covers the cavity like a reverse box is used to activate quadrupole term of FW-H equation. It is shown that adding a quadrupole term increases sound level in the high frequency range [8]. In 2017, Zafer and Konan studied the effect of cavityairfoil interaction with passive control on the acoustic signal.…”
Section: Introductionmentioning
confidence: 99%
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