EFFECT OF HYDROFOIL PLANFORM ON TIP VORTEX ROLL-UP AND CAVITATION

The effect of the planform of hydrofoils on tip vortex roll-up and cav itation has been investigated by testing three foils having the same N ACA 16020 cross section but different shapes. One foil has an elliptic al shape while the other two are shaped like quarters of ellipses; one with a straight leading edge and the other with a straight trailing e dge. Experiments were conducted in the ENSTA, Ecole Navale and IMHEF c avitation tunnels,with homologous foils of different sizes to investig ate Reynolds number effects. Hydrodynamic forces as well as cavitation inception and desinence performance were measured as a function of Re ynolds number and foil incidence angle. Laser Doppler measurements of the tangential and axial velocity profiles in the region immediately d ownstream of the tip were also performed. At equal incidence angle and Reynolds number, the three foils show different critical cavitation c onditions and the maximum tangential velocity near the tip increases a s the hydrofoil rip is moved from a forward to a rear position. Howeve r, the velocity profiles become more similar with increasing downstrea m distance, and at downstream distances greater than one chord aft of the tip, the differences between the foils disappear. The rate of tip vortex roll-lcp is much faster for the straight leading edge than for the straight trailing edge foil and, in the latter case, a significant portion of the roll-up occurs along the foil curved leading edge. The minimum of the pressure coefficient on the axis of the vortex was est imated from the velocity measurements and correlated with the desinent cavitation number for the largest free stream velocities. The correla tion of data is very satisfactory. Ar the highest Reynolds number test ed and at equal lift coefficients, the straight leading edge foil disp lays the most favorable cavitation desinent numbers.