TY - JOUR
T1 - Flow structures around a square cylinder
T2 - Effect of corner chamfering
AU - Hariprasad, C. M.
AU - Kumar, R. Ajith
AU - Dahl, Jason
AU - Sohn, Chang Hyun
N1 - Publisher Copyright:
© 2024 American Society of Civil Engineers.
PY - 2024/5/1
Y1 - 2024/5/1
N2 - In this paper, results of a flow visualization study on the flow around a square cylinder with corner chamfering are presented. The corners of the test cylinders were chamfered with each corner forming a triangle with chamfer dimension b. Experiments were conducted for b=Bo ratios of 0.05, 0.1, 0.2, and 0.3 where Bo is the side dimension of the uncut square cylinder. The flow structures, particularly the vortex shedding mode and mechanism around the uncut as well as chamfered square cylinders, were investigated in order to deduce the effect of corner modification. All the studies were conducted at a Reynolds number value of 2,100 (based on Bo) on both stationary and oscillating cylinders. For oscillating cases, a special mechanism was built to oscillate the cylinders (forced oscillation) at desired amplitudes and frequencies. Results indicates that corner chamfering brings notable changes in the near-wake flow structures of a square section cylinder both in stationary and oscillating conditions. In view of aerospace structures with similar geometries, the present results carry considerable practical significance.
AB - In this paper, results of a flow visualization study on the flow around a square cylinder with corner chamfering are presented. The corners of the test cylinders were chamfered with each corner forming a triangle with chamfer dimension b. Experiments were conducted for b=Bo ratios of 0.05, 0.1, 0.2, and 0.3 where Bo is the side dimension of the uncut square cylinder. The flow structures, particularly the vortex shedding mode and mechanism around the uncut as well as chamfered square cylinders, were investigated in order to deduce the effect of corner modification. All the studies were conducted at a Reynolds number value of 2,100 (based on Bo) on both stationary and oscillating cylinders. For oscillating cases, a special mechanism was built to oscillate the cylinders (forced oscillation) at desired amplitudes and frequencies. Results indicates that corner chamfering brings notable changes in the near-wake flow structures of a square section cylinder both in stationary and oscillating conditions. In view of aerospace structures with similar geometries, the present results carry considerable practical significance.
UR - http://www.scopus.com/inward/record.url?scp=85185801722&partnerID=8YFLogxK
U2 - 10.1061/JAEEEZ.ASENG-4404
DO - 10.1061/JAEEEZ.ASENG-4404
M3 - Article
AN - SCOPUS:85185801722
SN - 0893-1321
VL - 37
JO - Journal of Aerospace Engineering
JF - Journal of Aerospace Engineering
IS - 3
M1 - 04024021
ER -