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Calculations of Separated Vortex Flows at Low Speed for Low-Aspect-Ratio Wings

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Fluid Dynamics of High Angle of Attack

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Summary

An implicit finite-difference scheme has been developed for solving three-dimensional incompressible Navier-Stokes equations. Computations for complicated vortical flows past several sharp- and round-edged delta and double-delta wings at high angles of attack and sideslip are discussed. Computed results demonstrate the effectiveness of the present method and show good agreement with experimental data.

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Author information

Authors and Affiliations

  1. NASA Langley Research Center, Hampton, Virginia, USA

    C. H. Liu

  2. Vigyan, Inc., Hampton, Virginia, USA

    C.-H. Hsu

Authors
  1. C. H. Liu
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  2. C.-H. Hsu
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Editor information

Editors and Affiliations

  1. Dept. of Aeronautics Faculty of Engineering, The University of Tokyo, 7-3-1 Hongo, Bunkyo-ku Tokyo 113, Japan

    R. Kawamura  & Y. Aihara  & 

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© 1993 Springer-Verlag Berlin Heidelberg

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Liu, C.H., Hsu, CH. (1993). Calculations of Separated Vortex Flows at Low Speed for Low-Aspect-Ratio Wings. In: Kawamura, R., Aihara, Y. (eds) Fluid Dynamics of High Angle of Attack. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-52460-8_24

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  • DOI: https://doi.org/10.1007/978-3-642-52460-8_24

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-52462-2

  • Online ISBN: 978-3-642-52460-8

  • eBook Packages: Springer Book Archive

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