Yayın: İki Boyutlu Cisimler Etrafında Akım Gürültüsünün İncelenmesi
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Dosyalar
Tarih
Yazarlar
Danışman
Bölüm / Program
Gemi İnşaatı ve Gemi Makinaları Mühendisliği
Naval Architecture and Marine Engineering
Naval Architecture and Marine Engineering
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Fen Bilimleri Enstitüsü
Institute of Science and Technology
Institute of Science and Technology
Türü
Özet
Bu çalışmada, NACA 0012 foil yapısı etrafında akım gürültüsü sayısal yöntemler kullanılarak hesaplanmış, kanat hücum açısı ve kanat çıkış kenar yapısının akım gürültüsü üzerine olan etkileri iki boyutlu olarak incelenmiştir. Ayrıca dairesel silindir etrafında akım gürültüsü yöntem doğrulama aşamasında incelenmiştir. Cisim etrafındaki basınç değişimleri Navier Stokes denklemlerinin nümerik olarak çözülmesi ile elde edilmiş, denklemleri ayrıklaştırma yöntemi olarak hesaplamalı akışkanlar dinamiği alanında yaygın olarak kullanılan Sonlu Hacimler Yöntemi (FVM) kullanılmıştır. Akustik kaynaklar Lighthill analojisinden türetilmiş olan Curle ve Proudman yöntemleri kullanılarak incelenmiş, uzak alan gürültüsü "Ffowcs Williams and Hawkings (FW-H)" denklemleri kullanılarak hesaplanmıştır.
Aerodynamic noise can be defined as a sound generated by aerodynamic forces induced by flows. Flow noise around two dimensional geometries used in aerospace, automotive, wind turbine and marine industries has become very popular research topic. Lots of theoretical and experimental methods have been developed for noise prediction in the last two decades. In this study, the flow around NACA 0012 foil has been computed by using numerical techniques. Effects of angle of attack and the trailing edge form on the flow noise have been investigated in two-dimensions by Computational Fluid Dynamics (CFD) techniques. In finite volume computations a commercial software STAR CCM+ has been used. In order to validate this study, the flow noise around a circular cylinder has also been investigated. Far field noise was computed by using Ffowcs Williams and Hawkings (FW-H) equations. The analyses were done for different Reynolds numbers, different angle of attacks, in different mediums (water or air) and with different trailing edge forms (sharp, flat and circular trailing edges) in two-dimensional cases. The results have been compared with each other and the effects of Reynolds number and the trailing edge forms were investigatedwith different fluid types to obtain the noise spectral characteristics.
Aerodynamic noise can be defined as a sound generated by aerodynamic forces induced by flows. Flow noise around two dimensional geometries used in aerospace, automotive, wind turbine and marine industries has become very popular research topic. Lots of theoretical and experimental methods have been developed for noise prediction in the last two decades. In this study, the flow around NACA 0012 foil has been computed by using numerical techniques. Effects of angle of attack and the trailing edge form on the flow noise have been investigated in two-dimensions by Computational Fluid Dynamics (CFD) techniques. In finite volume computations a commercial software STAR CCM+ has been used. In order to validate this study, the flow noise around a circular cylinder has also been investigated. Far field noise was computed by using Ffowcs Williams and Hawkings (FW-H) equations. The analyses were done for different Reynolds numbers, different angle of attacks, in different mediums (water or air) and with different trailing edge forms (sharp, flat and circular trailing edges) in two-dimensional cases. The results have been compared with each other and the effects of Reynolds number and the trailing edge forms were investigatedwith different fluid types to obtain the noise spectral characteristics.
Tanım
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2014
Thesis (M.Sc.) -- İstanbul Technical University, Instıtute of Science and Technology, 2014
Thesis (M.Sc.) -- İstanbul Technical University, Instıtute of Science and Technology, 2014
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Haklar
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İTÜ theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission.
İTÜ theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission.
Anahtar Kelimeler
Hesaplamalı Akışkanlar Dinamiği (had) Hesaplamalı Aero Akustik (haa) Naca0012 Foil Ffowcs Williams Ve Hawkings, Computational Fluid Dynamics (cfd) Computational Aero Acoustics (caa) Naca0012 Foil Ffowcs Williams And Hawkings
Alıntı
Onay
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Tamamlayıcı Bilgiler
Referans Gösteren
10
Görüntülenme
107
İndirme
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