Reynolds-number-effects in flow around a rectangular cylinder with aspect ratio 1:5

The paper reports on experiments carried out over a wide range of Reynolds numbers in a high pressure wind tunnel. The model was a sharp-edged rectangular cylinder with aspect ratio height/width 1:5 (width/span ratio 1:10.8), which was investigated in both basic orientations, lengthwise (4×103<Re<4×105) and perpendicular to the flow (2.7×104<Re<6.4×105). The Reynolds number is based on the height of the model normal to the flow. Steady and unsteady forces were measured with a piezoelectric balance. Thus along with steady (i.e. time averaged values) including the base pressure coefficient, also power spectra and probability density functions were measured yielding for example Strouhal numbers, higher statistical moments, etc. A response diagram for the vortex resonance phenomenon was taken for the natural bending motion of the slender model. If lift coefficient for constant angle of attack is plotted against Reynolds number, a significant Reynolds number effect is seen. For α=4°, the curve shows an inflection point and the lift varies between 0.3 and 0.6. For α=6° and 2° there are similar variations shifted to lower and higher values of Re, respectively. Probably the shapes of separation bubbles that depend on the Reynolds number are responsible for these effects. No Reynolds number effects were observed when the long side was normal to the flow, an orientation where reattachment at the side walls is not possible. Comparing both basic cases (α=0° and 90°), the interpretation of the probability distributions of lift force leads to the conclusion that the possibility of reattachment (α=0°) seems to enhance the degree of order in the vortex shedding process.

[1]  G. Schewe Nonlinear flow-induced resonances of an H-shaped section , 1989 .

[2]  Claudio Mannini,et al.  Detached-Eddy Simulation of flow around a 1:5 rectangular cylinder , 2008 .

[3]  Gl Larose,et al.  On the Reynolds number sensitivity of the aerodynamics of bluff bodies with sharp edges , 2006 .

[4]  Allan Larsen Torsion Galloping of Elongated Bluff Cross Sections , 2002 .

[5]  Kenji Shimada,et al.  APPLICATION OF A MODIFIED k–ε MODEL TO THE PREDICTION OF AERODYNAMIC CHARACTERISTICS OF RECTANGULAR CROSS-SECTION CYLINDERS , 2002 .

[6]  A. N. Stokes,et al.  Flow-resonant sound interaction in a duct containing a plate, II: Square leading edge , 1986 .

[7]  Claudio Mannini,et al.  Three-Dimensional Numerical Simulation of Flow Around a 1 : 5 Rectangular Cylinder , 2009 .

[8]  W. A. Mair,et al.  Pressure Distributions and Forces on Rectangular and D-shaped Cylinders , 1972 .

[9]  Allan Larsen,et al.  Reynolds Number Effects in the Flow Around a Bluff Bridge Deck Cross Section , 1998 .

[10]  R. Parker,et al.  Effects of sound on flow separation from blunt flat plates , 1983 .

[11]  Yukio Ishida,et al.  Flow‐Induced Vibrations , 2012 .

[12]  Frank Thiele,et al.  Assessment of Explicit Algebraic Stress Models in Transonic Flows , 1999 .

[13]  Claudio Mannini,et al.  Unsteady RANS modelling of flow past a rectangular cylinder: Investigation of Reynolds number effects , 2010 .

[14]  Günter Schewe,et al.  Reynolds-number effects in flow around more-or-less bluff bodies , 2001 .

[15]  Günter Schewe Force and Moment Measurements in Aerodynamics and Aeroelsticity using Piezoelectric Transducers , 2007 .

[16]  M. Matsumoto,et al.  Spanwise Coherence Characteristics of Surface Pressure Field on 2-D Bluff Bodies , 2001 .

[17]  Yasuharu Nakamura,et al.  Vortex excitation of prisms with elongated rectangular, H and [vdash ] cross-sections , 1986, Journal of Fluid Mechanics.

[18]  Yasuaki Ito,et al.  Torsional flutter and branch characteristics for 2-D rectangular cylinders , 2005 .

[19]  P. W. Bearman,et al.  An Investigation of the Flow around Rectangular Cylinders , 1972 .

[20]  Hiroshi Nakaguchi,et al.  An Experimental Study on Aerodynamic Drag of Rectangular Cylinders , 1968 .

[21]  Spencer J. Sherwin,et al.  A numerical study of rotational and transverse galloping rectangular bodies , 2003 .

[22]  Walter G Vincenti,et al.  Wall interference in a two-dimensional-flow wind tunnel, with consideration of the effect of compressibility , 1944 .

[23]  A. Roshko Experiments on the flow past a circular cylinder at very high Reynolds number , 1961, Journal of Fluid Mechanics.

[24]  Noel K. Delany,et al.  Low-speed drag of cylinders of various shapes , 1953 .

[25]  Alberto Zasso,et al.  BARC: a Benchmark on the Aerodynamics of a Rectangular 5:1 Cylinder , 2009 .

[26]  Yasuharu Nakamura,et al.  TORSIONAL FLUTTER OF RECTANGULAR PRISMS , 1975 .

[27]  Claudio Mannini,et al.  Numerical investigation on the three-dimensional unsteady flow past a 5:1 rectangular cylinder , 2011 .

[28]  G. Schewe On the force fluctuations acting on a circular cylinder in crossflow from subcritical up to transcritical Reynolds numbers , 1983, Journal of Fluid Mechanics.

[29]  Yuji Ohya,et al.  Experiments on vortex shedding from flat plates with square leading and trailing edges , 1991, Journal of Fluid Mechanics.