Research Article

Effect of attack angle on the flow around adjacent circular and rectangular prisms

Volume: 10 Number: 2 July 27, 2021
EN TR

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

References

  1. K. Y. Billah and R. H. Scanlan, Resonance, Tacoma Narrows bridge failure, and undergraduate physics textbooks. American Journal of Physics, 59, 118–124, 1991. https://doi.org/10.1119/1.16590.
  2. A. C. Khanduri, T. Stathopoulos and C. Bédard, Wind-induced interference effects on buildings — a review of the state-of-the-art. Engineering Structures, 20 617–630, 1998. https://doi.org/10.1016/S0141-0296(97)00066-7.
  3. P. Burattini and A. Agrawal, Wake interaction between two side-by-side square cylinders in channel flow. Computers & Fluids, 77, 134–142, 2013. https://doi.org/10.1016/j.compfluid.2013.02.014.
  4. A. Roshko, Experiments on the flow past a circular cylinder at very high Reynolds number. Journal of Fluid Mechanics, 10, 345–356, 1961. https://doi.org/10.1017/S0022112061000950
  5. Y. Bao and J. Tao, The passive control of wake flow behind a circular cylinder by parallel dual plates. Journal of Fluids and Structures, 37, 201–219, 2013. https://doi.org/10.1016/j.jfluidstructs.2012.11.002.
  6. S. Shukla, R. N. Govardhan and J. H. Arakeri, Flow over a cylinder with a hinged-splitter plate. Journal of Fluids and Structures, 25, 713–720, 2009. https://doi.org/10.1016/j.jfluidstructs.2008.11.004.
  7. E. A. Anderson and A. A. Szewczyk, Effects of a splitter plate on the near wake of a circular cylinder in 2 and 3-dimensional flow configurations. Experiments in Fluids, 23, 161–174, 1997. https://doi.org/10.1007/s003480050098.
  8. T. Igarashi, Drag reduction of a square prism by flow control using a small rod. Journal of Wind Engineering and Industrial Aerodynamics, 69,141–153, 1997. https://doi.org/10.1016/S0167-6105(97)00150-5

Details

Primary Language

English

Subjects

Mechanical Engineering

Journal Section

Research Article

Publication Date

July 27, 2021

Submission Date

March 10, 2021

Acceptance Date

June 16, 2021

Published in Issue

Year 2021 Volume: 10 Number: 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. NOHU J. Eng. Sci. 2021;10(2):833-839. doi:10.28948/ngumuh.894558
Chicago
Seyhan, Mehmet, Mustafa Sarıoğlu, and 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 (July 1, 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, and Y. E. Akansu, “Effect of attack angle on the flow around adjacent circular and rectangular prisms”, NOHU J. Eng. Sci., vol. 10, no. 2, pp. 833–839, July 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 (July 1, 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. NOHU J. Eng. Sci. 2021;10:833–839.
MLA
Seyhan, Mehmet, et al. “Effect of Attack Angle on the Flow Around Adjacent Circular and Rectangular Prisms”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi, vol. 10, no. 2, July 2021, pp. 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. NOHU J. Eng. Sci. 2021 Jul. 1;10(2):833-9. doi:10.28948/ngumuh.894558