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Flow Visualization Study of Vortex Breakdown on a 65° Delta Wing in Dynamic Motion Regime

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Flow Visualization VI

  • 354 Accesses

Abstract

An application of helium-bubble technique has been attempted in order to investigate the behaviour of the vortical structures on a delta wing in oscillatory conditions.

The dynamic behaviour of the vortex breakdown phenomenon has been analyzed.

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References

  1. Jarrah M. A. M., “Low Speed Wind Tunnel Investigation of Flow About Delta Wing, Oscillating in Pitch to Very High Angle of Attack” AIAA 89-0295, Jan. 1989

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  2. Cunningham Jr. A. M., “Unsteady Low Speed Wind Tunnel Test of a Straked Delta Wing, Oscillating in Pitch” AFWAL TR-87-3098, April 1988

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  4. Brandon J. M., “Effect of Large Amplitude Pitching Motions on the Unsteady Aerodynamic Characteristics of Flat-plate Wings” AIAA 88-4331, August 1988

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  5. Lee M., “Vortex Dynamics of Delta Wings” L. N. E., Vol. 46, 1989 Springer Verlag, Berlin

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  6. Ashley H., “Unsteady Aerodynamic Loading of Delta Wings for Low and High Angles of Attack” Proc. Int. Symp. on Non-steady Fluid Dynamics, June 1990

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  7. Hanff E. S., “Oscillatory Test Techniques” AGARD-R-776, April 1991

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  8. Hanff E. S., “Large Amplitude Oscillations” AGARD-R-776, April 1991

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  9. Guglieri G., Onorato M., Quagliotti F. “Untersuchung des Wirbelaufplatzens an Deltaflügeln”, Zeitschrift fur Flugwiss., n. 16-4, 1992

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Author information

Authors and Affiliations

  1. Centro Studi Dinamica Fluidi, CNR, Torino, Italy

    G. Guglieri

  2. Aerospace Engineering Dept, Turin Polytechnic Institute, Technical University, Torino, Italy

    M. Onorato & F. Quagliotti

Authors
  1. G. Guglieri
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  2. M. Onorato
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  3. F. Quagliotti
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Editor information

Editors and Affiliations

  1. Dept. of Mechanical Engineering, Tokai University, Kitakaname, Hiratsuka Kanagawa, 259-12, Japan

    Yoshimichi Tanida

  2. Dept. of Mechanical Systems Engineering, Toyama Prefectural University, Kosugi-machi Toyama, 939-03, Japan

    Hiroshi Miyashiro

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© 1992 Springer-Verlag Berlin Heidelberg

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Guglieri, G., Onorato, M., Quagliotti, F. (1992). Flow Visualization Study of Vortex Breakdown on a 65° Delta Wing in Dynamic Motion Regime. In: Tanida, Y., Miyashiro, H. (eds) Flow Visualization VI. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-84824-7_43

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  • DOI: https://doi.org/10.1007/978-3-642-84824-7_43

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-84826-1

  • Online ISBN: 978-3-642-84824-7

  • eBook Packages: Springer Book Archive

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