Experimental Characterization of High-Amplitude Fluid–Structure Interaction of a Flexible Hydrofoil at High Reynolds Number

Author:

Elbing Brian R.1,Young Steven D.2,Jonson Michael L.3,Campbell Robert L.4,Craven Brent A.5,Kunz Robert F.6,Koudela Kevin L.7

Affiliation:

1. School of Mechanical and Aerospace Engineering, Oklahoma State University, 201 General Academic Building, Stillwater, OK 74078

2. Applied Research Laboratory, Pennsylvania State University, 3210B Garfield Thomas Water Tunnel, University Park, PA 16802

3. Applied Research Laboratory, Pennsylvania State University, 3200B Garfield Thomas Water Tunnel, University Park, PA 16802

4. Applied Research Laboratory, Pennsylvania State University, 300R Garfield Thomas Water Tunnel, University Park, PA 16802

5. Applied Research Laboratory, Department of Mechanical and Nuclear Engineering, Pennsylvania State University, University Park, PA 16802

6. Department of Mechanical and Nuclear Engineering, Pennsylvania State University, 301C Reber Building, University Park, PA 16802

7. Applied Research Laboratory, Pennsylvania State University, 155 Applied Research Laboratory, University Park, PA 16802

Abstract

Abstract A fluid–structure interaction (FSI) experiment was performed to study low-frequency (∼10 Hz), high-amplitude (±3.5% of the span) fin motion. This was achieved by placing an Inconel swept-fin at −9.6 deg angle-of-attack within the wake of a roughened cylinder. Speeds between 2.5 and 3.6 m/s produced cylinder diameter-based Reynolds numbers between 190,000 and 280,000, respectively. Detailed descriptions of the geometry, material/structural behavior, fluid properties, and initial conditions are provided to facilitate computational model development. Given the initial conditions, the resulting forced fin behavior was characterized with measurements of the mean and fluctuating velocity upstream of the fin (i.e., within the cylinder wake), fin tip/surface motion, and fin constraint forces/moments. This work provides a detailed experimental dataset of conditions mimicking a crashback event that is also a challenging FSI benchmark problem involving turbulent, vortex-induced structure motion. It has been used as a validation condition for FSI simulations, and it can be used to validate other FSI models as well as identifying strengths and weaknesses of various modeling approaches.

Funder

Defense Advanced Research Projects Agency

Publisher

ASME International

Subject

General Engineering

Reference50 articles.

1. Bridges, D. H. , 2004, “A Detailed Study of the Flow Field of a Submarine Propeller During a Crashback Maneuver,” Mississippi State University, Technical Report MSSU-ASE-04-1.

2. Unsteady Propeller Performance in Crashback Conditions With and Without a Duct;Jessup,2006

3. Large Eddy Simulation of Crashback in Marine Propellers;Vyšohlíd,2006

4. Prediction of High-Amplitude Forces During Propeller Crashback;Chang,2008

5. Experimental Investigation of the Submarine Crashback Maneuver;Bridges;J. Fluid. Eng.,2008

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