======Plane Wake after a Circular Cylinder====== =====Experiments by Antonia and Browne===== ---- ====Description==== Plane turbulent wake downstream of a heated circular cylinder. A 2D flow with temperature as passive scalar. ===Geometry and Flow Characteristics==== The wake-generating body is a stainless steel tube of \(d = 2.67\) mm outer diameter. It is mounted horizontally in the mid-plane of the working section of the wind tunnel, with its axis located at \(x = 0\) and \(y = 0\). Electrical heating of the cylinder provides the temperature as a passive marker of the flow in the self-preserving region, and a zero longitudinal pressure gradient prevents free-stream velocity variations. For computations, it is suggested that uniform inlet conditions are applied upstream of the cylinder at around \(x/d=-10\), and the domain should extend to at least \(x/d = 420\), where measurements are provided, as shown in . {{ figs:case003:case03-geom.png | Flow geometry}} ===Flow Parameters=== Air with: * Kinematic viscosity: \(\nu =1.53 \times 10^{-5}\) m2/s. * Free-stream velocity: \(U_e = 6.70\) m/s. * Reynolds number based on \(d\): \(Re_d = 1170\). At station \(x/d = 420\): * Mean-velocity defect half-width: \(L = 12.3\) mm * Centreline mean-velocity defect: \(U_o = 0.36\) m/s * Relative mean-temperature excess: \(T_o = 0.82\)oC Constant power supplied for the electrical heating of the cylinder: 100 W. ===Inflow Conditions=== At station \(x/d\) = -10, constant velocity \(U_e\) and temperature. Turbulent quantities corresponding to a free-stream turbulence level of 0.08%. ====Experimental Details==== Velocity measurements were taken using either single hot wires and single X-wires, or two single hot wires or two X-wires, in order to obtain various turbulence quantities. Temperature measurements were made using cold-wire probes. ===Measurement Errors=== * \(\delta(\overline{vt}/(U_oT_o)) = 12\)% * \(\delta(\text{positions}) = \pm 0.02\) m ====Available Measurements==== ===Velocity Measurements:=== At station \(x/d = 420\), profiles for \(\eta = y/L\) ranging from 0 to 2.2 of: * First order moment: \(U/U_o\) and \((U_e-U)/U_o\) * Reynolds stresses: \(\overline{u^2}/U_o^2\), \(\overline{v^2}/U_o^2\), \(\overline{w^2}/U_o^2\) * Turbulent kinetic energy: \(k/U_o^2\) * Turbulent kinetic energy dissipation rates: \(\varepsilon L/U_o^3\), \(\varepsilon_{homogeneous} L/U_o^3\) * Third order moment: Part of the diffusion term of the \(k\) transport equation: \(d(\overline{u_ku_kv}/2)/d\eta\) ===Temperature Measurements=== At station \(x/d=420\), profiles for \(\eta = y/L\) from 0 to 2.5 of: * First order moment: \((T-T_e)/T_o\) * Second order moments: \(\overline{t^2}/T_o^2\), \(\overline{vt}/(U_oT_o)\) * Dissipation rate: \(\varepsilon_{t} L/(U_oT_o^2)\) * Third order moment: Part of the diffusion term of the \(\overline{t^2}\) transport equation: \(d(\overline{vt^2}/2)/d\eta\) [[case003-plots|Sample plots]] of some of these quantities are available. The data can be downloaded as compressed archive files from the links below, or as individual files. * {{cdata:case003:pwc-allfiles.zip|pwc-allfiles.zip}} * {{cdata:case003:pwc-allfiles.tar.gz|pwc-allfiles.tar.gz}} The individual files provided are: * Dynamic field profiles, contained in the file {{cdata:case003:dynamic-field-data.dat|dynamic-field-data.dat}} * Thermal field profiles, contained in the file {{cdata:case003:thermal-field-data.dat|thermal-field-data.dat}} * Additional notes in {{cdata:case003:readme.txt|readme.txt}} ====Main References==== - Browne, L.W.B., Antonia, R.A., Shah, D.A. (1987). [[https://doi.org/10.1017/S002211208700154X|Turbulent energy dissipation in a wake]]. //J. Fluid Mech.//, Vol. 179, pp. 307-326. - Antonia, R.A., Browne, L.W.B. (1986). [[https://doi.org/10.1017/S0022112086002343|Anisotropy of the temperature dissipation in a turbulent wakei]]. //J. Fluid Mech.//, Vol. 163, pp. 393-403. - Antonia, R.A., Browne, L.W.B. (1986). [[https://doi.org/10.1016/0017-9310(86)90073-6|Heat transport in a turbulent plane wake]]. //Int. J. Heat Mass Transfer//, Vol. 29, pp. 1585-1592. - Antonia, R.A., Browne, L.W.B., Fulachier, L. (1987). [[https://doi.org/10.1007/BF00277708|Average wavelength of organised structures in the turbulent far wake of a cylinder]]. //Expts. in Fluids//, Vol. 5, pp. 298-304. ---- Indexed data: case : 003 title : Plane Wake after a Circular Cylinder author* : Antonia, Browne year : 1985 type : EXP flow_tag* : wake, scalar