Journal article
Unsteady free-surface wave-induced boundary-layer separation for a surface-piercing NACA 0024 foil : Towing tank experiments
Journal of fluids and structures, Vol.22(1), pp.77-98
2006
DOI: 10.1016/j.jfluidstructs.2005.09.004
Abstract
Unsteady free-surface, wave-induced separation is documented using towing tank experiments for a surface-piercing NACA 0024 foil, which has insignificant separation, no wave effects, and 2-D flow in the deep. The test conditions are for minimal, reattaching, and nonreattaching separation: Froude numbers , 0.37, and 0.55 and Reynolds , 1.52, and 2.26×106. The measurements include mean far-field wave elevations for all three Fr, unsteady near-field wave elevations for medium and low Fr, mean foil-surface pressures for all three Fr, and unsteady foil-surface pressures for medium Fr. Unsteady measurements are statistically analyzed for mean, r.m.s., FFT, PSD, and phased-averaged organized oscillations and random fluctuation components. For , there is no separation and the expected Kelvin waves are present. For , the separation on the free and foil surfaces is demarcated by large r.m.s. (15–20% of the mean value dynamic range) and 1.94, 0.82, and 0.30 Hz dominant FFT frequency regions corresponding to shear layer, Karman shedding, and flapping instabilities, respectively. A large bow wave resembles a spilling breaker with low r.m.s. (2–5% of the mean value dynamic range) and 8.5 Hz dominant FFT frequency on the free and foil surfaces. Mean wave elevations in the separation region are relatively constant with intense free-surface oscillations, turbulence, and breaking. Outside the separation and wake region, the Kelvin waves are evident. The foil-surface pressure is high in the bow wave, low in the wave trough, gradually rises towards the trailing edge, and recovers 2-D distributions at large depths. For , the bow wave is enormous. The separation region moves towards the trailing edge with increased splashing and bubbles. The Kelvin waves are no longer distinguishable due to increased free-surface turbulence. The mean foil-surface pressure, free-surface, and bottom effects interact with each other. The combination of the present albeit relatively sparse experimental data with complementary computational fluid dynamics studies provides a credible description of the flow physics.
Details
- Title: Subtitle
- Unsteady free-surface wave-induced boundary-layer separation for a surface-piercing NACA 0024 foil : Towing tank experiments
- Creators
- B METCALF - IIHR-Hydroscience & Engineering, The University of Iowa, 100 C. Maxwell Stanley Hydraulics Laboratory, Iowa City, IA 52242-1585, United StatesJ LONGO - IIHR-Hydroscience & Engineering, The University of Iowa, 100 C. Maxwell Stanley Hydraulics Laboratory, Iowa City, IA 52242-1585, United StatesS GHOSH - IIHR-Hydroscience & Engineering, The University of Iowa, 100 C. Maxwell Stanley Hydraulics Laboratory, Iowa City, IA 52242-1585, United StatesF STERN - IIHR-Hydroscience & Engineering, The University of Iowa, 100 C. Maxwell Stanley Hydraulics Laboratory, Iowa City, IA 52242-1585, United States
- Resource Type
- Journal article
- Publication Details
- Journal of fluids and structures, Vol.22(1), pp.77-98
- Publisher
- Elsevier; London
- DOI
- 10.1016/j.jfluidstructs.2005.09.004
- ISSN
- 0889-9746
- eISSN
- 1095-8622
- Language
- English
- Date published
- 2006
- Academic Unit
- Mechanical Engineering
- Record Identifier
- 9984064249202771
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