Improvement of Hydrofoil Performance by Partial Ventilated Cavitation in Steady Flow and Periodic Gusts

Author:

Kopriva Jim1,Arndt Roger E. A.1,Amromin Eduard L.2

Affiliation:

1. Saint Anthony Falls Laboratory, University of Minnesota Minneapolis, MN 55414

2. Mechmath LLC, Prior Lake, MN 55372

Abstract

This paper describes a study of the response of a recently developed low-drag partially cavitating hydrofoil (denoted as OK-2003) to periodical perturbations of incoming flow. A two-flap assembly specially designed to simulate sea wave impact on the cavitating hydrofoil generates the perturbations. The design range of cavitation number was maintained by ventilation. Unsteady flow can be simulated over a range of ratios of gust flow wavelength to cavity length. The measurement of time-average lift and drag coefficients and their fluctuating values over a range of inflow characteristics allows a determination of hydrofoil performance over a range of conditions that could be expected for a prototype hydrofoil. Both regular interaction with practically linear perturbations and resonancelike singular interaction with substantial nonlinear effects were noted. The observations are accompanied by a numerical analysis that identifies resonance phenomena as a function of excitation frequency.

Publisher

ASME International

Subject

Mechanical Engineering

Reference13 articles.

1. Investigation of a Low-Drag Partially Cavitating Hydrofoil;Amromin

2. Hydrofoil Drag Reduction by Partial Cavitation;Amromin;ASME J. Fluids Eng.

3. Reichardt, H. , 1946, “The Law of Cavitation Bubbles at Axially Symmetric Bodies in a Flow,” Ministry of Aircraft Production, Report and Translation No. 766.

4. Experimental Studies of Ventilated Cavities on Dynamic Test Model;Kuklinski

5. Schiebe, F. R., and Wetzel, J. M., 1964, “Further Studies of Ventilated Cavities on Submerged Bodies,” University of Minnesota—SAFL, Project Report No. 72.

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