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Experimental investigation of combined vibrations for a hydrofoil-rod system at low Reynold numbers

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Abstract

A hydrodynamic tunnel experimental investigation and analysis of vibration characteristics for a hydrofoil in a transient regime is considered. Tests are performed for NACA 0017 models with a non-uniform section at an angle of attack AOA = 5º and Reynolds numbers up to Re = 7.0 × 106. This study is related to a project design of experiments in a complex facility that involves several parameters. The analysis focuses on the vibrations of a hydrofoil for different values of the bracing stiffness kh, the torsional stiffness ka, and the locations of the elastic axis ā and of the center of gravity xa. The structural bracing response is investigated via measurements of the displacement of the free tip section of the hydrofoil using a three-axis acceleration sensor, and the torsional response of the structure is analyzed via measurements of displacements with single-axis acceleration sensors. The hydrofoil is made of reinforced plastics without flexibility, and elastic functions are provided by a spring support mechanism combined with a torsional structure. The study shows that an increase of the velocity V results in different behaviors of the bracing and torsional amplitudes. Another notable result of the study is that the emergence of transition occurs simultaneously with additional peaks and changes of vibration amplitudes.

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References

  1. Caster M. The structure and behavior of separation bubbles [R], Revised Aero Report, 1967, 1181.

    Google Scholar 

  2. Rojratsirikul P., Genc M. S., Wang Z., et al. Flow–induced vibrations of low aspect ratio rectangular membrane wings [J], Journal of Fluids and Structures, 2011, 27(8): 1296–1309.

    Article  Google Scholar 

  3. Lian Y., Shyy W., Viieru D., et al. Membrane wing aerodynamics for micro air vehicles [J], Progress in Aerospace Sciences, 2003, 39(6): 425–465.

    Article  Google Scholar 

  4. Lian Y., Shyy W. Laminar–turbulent transition of a low reynolds number rigid or flexible airfoil [J], AIAA journal, 2007, 45(7): 1501–1513.

    Article  Google Scholar 

  5. Hu H., Yang Z. An experimental study of the laminar flow separation on a low–reynolds–number airfoil [J], Journal of Fluids Engineering, 2008, 130(5): 051101.

    Article  Google Scholar 

  6. Rist U., and Maucher U. Investigations of time–growing instabilities in laminar separation bubbles [J], European Journal of Mechanics–B/Fluids, 2002, 21(5): 495–509.

    Article  MATH  Google Scholar 

  7. Gostelow J. P., McMullan W. A., Walker G J. Streamwise vorticity, laminar separation and transition in flows over turbomachinery blades [C]. 49th AIAA Aerospace Science Meeting, AIAA, 2011, volume 285.

    Google Scholar 

  8. Ravi S., Watkins S., Watmuff J., et al. Transient loads occurring over a thin airfoil subjected to large–scale freestream turbulence [J], AIAA Journal, 2013, 51(6): 1473–1485.

    Article  Google Scholar 

  9. Nati A., Kat R. D., Scarano F., et al. Dynamic pitching effect on a laminar separation bubble [J], Experiments in Fluids, 2015, 56(9): 1–17.

    Article  Google Scholar 

  10. Samson A., Sarkar S. An experimental investigation of a laminar separation bubble on the leading–edge of a modelled aerofoil for different reynolds numbers [J], Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2015, 0954406215594826.

    Google Scholar 

  11. DeMauro E. P., DellOrso H., Zaremski S., et al. Control of laminar separation bubble on naca 0009 airfoil using electroactive polymers [J], AIAA Journal, 2015, 53(8): 2270–2279.

    Article  Google Scholar 

  12. Garcia E, Yu P, Durgesh V, et al. Experimental Study of Thin and Thick Airfoils at Low Reynolds Numbers [C]. 54th AIAA Aerospace Sciences Meeting, 2016: 0854.

    Book  Google Scholar 

  13. Lambert A, Yarusevych S V. Analyzing Vortex Dynamics in the Laminar Separation Bubble vis Surface Pressure Measurements[C]. 45th AIAA Fluid Dynamics Conference, 2015: 2628.

    Book  Google Scholar 

  14. Lambert A. Vortex Dynamics within the Laminar Separation Bubble over a NACA 0018 Airfoil at Low Reynolds Numbers [D]. University of Waterloo, 2015.

    Google Scholar 

  15. Herr R W. A study of flutter at low mass ratios with possible application to hydrofoils [R]. National Aeronautics and Space Administration, Washington DC, 1961.

    Google Scholar 

  16. Ducoin A, Astolfi J A, Gobert M L. An experimental study of boundary–layer transition induced vibrations on a hydrofoil [J], Journal of Fluids and Structures, 2012, 32: 37–51.

    Article  Google Scholar 

Download references

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Correspondence to Yun-xiang You.

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Project supported by the National Natural Science Foundation of China (Grant No. 11802176).

Biography: Ren-feng Wang (1981-), Male, Ph. D.

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Wang, Rf., Chen, K., Nobelesse, F. et al. Experimental investigation of combined vibrations for a hydrofoil-rod system at low Reynold numbers. J Hydrodyn 31, 512–521 (2019). https://doi.org/10.1007/s42241-018-0151-1

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  • DOI: https://doi.org/10.1007/s42241-018-0151-1

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