Observations of Cavitation on a Three-dimensional Oscillating Hydrofoil
نویسندگان
چکیده
A test apparatus was designed and constructed to observe the effect of sinusoidal pitching oscillations on the cavitation of thredimensional hydrofoils. The apparatus is capable of oscillating hydrofoils at a rate up to 50 Hz and provides for adjustments in oscillation amplitude and mean angle of attack. Observations of the effect of pitching oscillation on cavitation have been made for a NACA 64-309 (modified) hydrofoil operating a its designed mean angle of attack of 7O with an oscillation amplitude of 2O. Photographs illustrating the interaction between natural cavity shedding frequencies and the foil reduced frequency are included. Nomenclature c = Foil chord length, 0.154m (6in) j = Excitation frequency in Hz k = Reduced frequency = wc/2Um P, = Water vapor pressure in kPa Pm = LTWT test section pressure in kPa Re = Reynolds number = Umc/v U, = LTWT test section velocity in m/s w -= Foil excitation frequency in rad/s a! = Hydrofoil angle of attack in degrees v = Kinematic viscosity in m2/s p = Fluid density in kg/m3 a = Cavitation number = (Pm P , ) / ( O . S ~ U ~ )
منابع مشابه
On the Dynamics and Acoustics of Cloud Cavitation on an Oscillating Hydrofoil
Observations have been made of the growth and collapse of surface and cloud cavitation on a finite aspect ratio hydrofoil oscillating in pitch. The cavitation was recorded using both still and high-speed motion picture photography, and the variations with cavitation number and reduced frequency of oscillation were investigated. The noise generated by the cavity collapse was also measured and an...
متن کاملCalculation of Three-dimensional Unsteady Sheet Cavitation by a Simple Suraface Panel Method “sqcm”
This paper presents a calculation method for the 3-D unsteady cavitating hydrofoil problem. The method is based on a simple surface panel method “SQCM” which satisfies easily the Kutta condition even in the unsteady problem. This method is applied to the Wagner problem, heaving hydrofoil and the hydrofoil in sinusoidal gust. We show some calculated results for partially cavitating and supercavi...
متن کاملOn the Detachment of a Leading Edge Cavitation
In the present paper we present an experimental investigation of the onset and detachment of leading edge cavitation. Tests are conducted in the LMH high speed cavitation tunnel on a 2-D Naca0009 hydrofoil having 100 mm chord length. Both Particle Image Velocimetry and flow visualisation are conducted for different test conditions. At low incidence angles, in the case of non cavitating flow, th...
متن کاملNumerical and experimental research on unsteady cavitating flow around NACA 2412 hydrofoil
This work deals with the numerical and experimental investigation of unsteady cavitating flow around a prismatic NACA 2412 hydrofoil. The main attention is focussed on the dependence of cavitation dynamics on the cavitation number at high incidence angles. The experimental research is carried out in the cavitation water tunnel the rectangular test section of which has inner dimensions 150×150×5...
متن کاملNumerical Investigation into Effects of Viscous Flux Vectors on Hydrofoil Cavitation Flow and Its Radiated Flow Noise
In this study, cavitation flow around a hydrofoil and its radiated hydro-acoustic fields were numerically investigated, with an emphasis on the effects of viscous flux vectors. The full three-dimensional unsteady compressible Reynolds-averaged Navier–Stokes equations were numerically solved. The mass transfer model was adopted to model phase changes between liquid water and vapor. To resolve th...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
عنوان ژورنال:
دوره شماره
صفحات -
تاریخ انتشار 2004