Flow separation in a straight draft tube, particle image velocimetry

27th IAHR Symposium on Hydraulic Machinery and Systems

Duquesne, P.^1 ; Maciel, Y.^1 ; Ciocan, G.D.^1 ; Deschênes, C.^1

Hydraulic Machine LAboratory (LAMH), Department of Mechanical Engineering, Laval University, 1065 avenue de la medicine, Québec

G1V 0A6, Canada^1

关键词: Best efficiency point;    Hydraulic machines;    Measurement planes;    Particle image velocimetries;    Recirculation regions;    Recirculation zones;    Tuft visualizations;    Two-component particles;   

Others  :  https://iopscience.iop.org/article/10.1088/1755-1315/22/3/032004/pdf
DOI  :  10.1088/1755-1315/22/3/032004

来源: IOP

【 摘 要 】

As part of the BulbT project, led by the Consortium on Hydraulic Machines and the LAMH (Hydraulic Machine Laboratory of Laval University), the efficiency and power break off in a bulb turbine has been investigated. Previous investigations correlated the break off to draft tube losses. Tuft visualizations confirmed the emergence of a flow separation zone at the wall of the diffuser. Opening the guide vanes tends to extend the recirculation zone. The flow separations were investigated with two-dimensional and two-component particle image velocimetry (PIV) measurements designed based on the information collected from tuft visualizations. Investigations were done for a high opening blade angle with a N11 of 170 rpm, at best efficiency point and at two points with a higher Q11. The second operating point is inside the efficiency curve break off and the last operating point corresponds to a lower efficiency and a larger recirculation region in the draft tube. The PIV measurements were made near the wall with two cameras in order to capture two measurement planes simultaneously. The instantaneous velocity fields were acquired at eight different planes. Two planes located near the bottom wall were parallel to the generatrix of the conical part of the diffuser, while two other bottom planes diverged more from the draft tube axis than the cone generatrix. The last four planes were located on the draft tube side and diverged more from the draft tube axis than the cone generatrix. By combining the results from the various planes, the separation zone is characterized using pseudo-streamlines of the mean velocity fields, maps of the Reynolds stresses and maps of the reverse-flow parameter. The analysis provides an estimation of the separation zone size, shape and unsteady character, and their evolution with the guide vanes opening.