TY - JOUR
T1 - Numerical simulation about the second instability in the two-dimensional laminar flow past a rotating circular cylinder
AU - Wang, Dan
AU - Yu, Yong
N1 - Publisher Copyright:
© 2015, Beijing Institute of Technology. All right reserved.
PY - 2015/11/1
Y1 - 2015/11/1
N2 - A numerical simulation method was taken to simulate the state that the flow was changing with Reynolds number and speed when a rotating circular cylinder was placed in a uniform stream. A comprehensive description was made to analyze the second instability state led by a rotating circular cylinder. The Reynolds numbers were set as Re=60, 80, 100, 130, 160, 240 with an increasing rotational speed until the flow was stable again. The different effect was analyzed and compared for the aerodynamic forces on the surface of cylinder, vorticity and the flow field around the cylinder in the first and second region of instability. The results show that when the flow is unstable with low rotational speeds, the critical rotational speeds are respectively α=1.40, 1.70, 1.80, 1.85, 1.90, 1.91 for the Reynolds numbers Re=60, 80, 100, 130, 160, 240. And in higher rotational speeds, the flow turns into unstable again and the related speed ranges are 5.1<α<5.6, 4.9<α<5.4, 4.6<α<5.2, 4.4<α<5.0, 4.3<α<4.9, 4.2<α<5.7 respectively.
AB - A numerical simulation method was taken to simulate the state that the flow was changing with Reynolds number and speed when a rotating circular cylinder was placed in a uniform stream. A comprehensive description was made to analyze the second instability state led by a rotating circular cylinder. The Reynolds numbers were set as Re=60, 80, 100, 130, 160, 240 with an increasing rotational speed until the flow was stable again. The different effect was analyzed and compared for the aerodynamic forces on the surface of cylinder, vorticity and the flow field around the cylinder in the first and second region of instability. The results show that when the flow is unstable with low rotational speeds, the critical rotational speeds are respectively α=1.40, 1.70, 1.80, 1.85, 1.90, 1.91 for the Reynolds numbers Re=60, 80, 100, 130, 160, 240. And in higher rotational speeds, the flow turns into unstable again and the related speed ranges are 5.1<α<5.6, 4.9<α<5.4, 4.6<α<5.2, 4.4<α<5.0, 4.3<α<4.9, 4.2<α<5.7 respectively.
KW - Critical rotational speed
KW - Lift and drag coefficient
KW - Rotating circular cylinder
KW - The second instability state
KW - Vorticity
UR - http://www.scopus.com/inward/record.url?scp=84954308443&partnerID=8YFLogxK
U2 - 10.15918/j.tbit1001-0645.2015.11.001
DO - 10.15918/j.tbit1001-0645.2015.11.001
M3 - Article
AN - SCOPUS:84954308443
SN - 1001-0645
VL - 35
SP - 1101
EP - 1107
JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
JF - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
IS - 11
ER -