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Effect of attack angle on the flow around adjacent circular and rectangular prisms
Abstract
An experimental investigation has been carried out to clarify the flow structure around adjacent circular and rectangular prisms. The measurements of hot-wire for Re= 4.1 x 10³, 9.0 x 10³ and 1.5 x 10⁴, lift and drag force for Re = 1.0 x 10⁴, and in addition the flow visualization experiments for Re = 2.3 x 10³ have been performed in the range of 0° ≤ α ≤ 180°. The adjacent bodies consist of a circular cylinder having 9.5 mm diameter and a rectangular prism having 6 mm x 10 mm cross-section attached to the circular cylinder from its short side in all the cases. The hot wire measurement results showed that the Strouhal number has Reynolds number independence for Re = 4.1x10³, 9.0x10³, and 1.5x10⁴. Sudden peaks in St and lift coefficients are obtained for a similar reason that is reattachment of the separated shear layer in the vicinity of α = 60° and 174°. For the adjacent bodies compared with the bare circular cylinder, 40%, and 25% drag reduction is obtained at α = 0° and 174°, respectively. The obtained results show that the variations of lift coefficient, drag coefficient, and Strouhal number are strictly subjected to the attack angle.
Keywords
Kaynakça
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Ayrıntılar
Birincil Dil
İngilizce
Konular
Makine Mühendisliği
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
27 Temmuz 2021
Gönderilme Tarihi
10 Mart 2021
Kabul Tarihi
16 Haziran 2021
Yayımlandığı Sayı
Yıl 2021 Cilt: 10 Sayı: 2
APA
Seyhan, M., Sarıoğlu, M., & Akansu, Y. E. (2021). Effect of attack angle on the flow around adjacent circular and rectangular prisms. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi, 10(2), 833-839. https://doi.org/10.28948/ngumuh.894558
AMA
1.Seyhan M, Sarıoğlu M, Akansu YE. Effect of attack angle on the flow around adjacent circular and rectangular prisms. NÖHÜ Müh. Bilim. Derg. 2021;10(2):833-839. doi:10.28948/ngumuh.894558
Chicago
Seyhan, Mehmet, Mustafa Sarıoğlu, ve Yahya Erkan Akansu. 2021. “Effect of attack angle on the flow around adjacent circular and rectangular prisms”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 10 (2): 833-39. https://doi.org/10.28948/ngumuh.894558.
EndNote
Seyhan M, Sarıoğlu M, Akansu YE (01 Temmuz 2021) Effect of attack angle on the flow around adjacent circular and rectangular prisms. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 10 2 833–839.
IEEE
[1]M. Seyhan, M. Sarıoğlu, ve Y. E. Akansu, “Effect of attack angle on the flow around adjacent circular and rectangular prisms”, NÖHÜ Müh. Bilim. Derg., c. 10, sy 2, ss. 833–839, Tem. 2021, doi: 10.28948/ngumuh.894558.
ISNAD
Seyhan, Mehmet - Sarıoğlu, Mustafa - Akansu, Yahya Erkan. “Effect of attack angle on the flow around adjacent circular and rectangular prisms”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 10/2 (01 Temmuz 2021): 833-839. https://doi.org/10.28948/ngumuh.894558.
JAMA
1.Seyhan M, Sarıoğlu M, Akansu YE. Effect of attack angle on the flow around adjacent circular and rectangular prisms. NÖHÜ Müh. Bilim. Derg. 2021;10:833–839.
MLA
Seyhan, Mehmet, vd. “Effect of attack angle on the flow around adjacent circular and rectangular prisms”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi, c. 10, sy 2, Temmuz 2021, ss. 833-9, doi:10.28948/ngumuh.894558.
Vancouver
1.Mehmet Seyhan, Mustafa Sarıoğlu, Yahya Erkan Akansu. Effect of attack angle on the flow around adjacent circular and rectangular prisms. NÖHÜ Müh. Bilim. Derg. 01 Temmuz 2021;10(2):833-9. doi:10.28948/ngumuh.894558