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

  • C. H. Liu
  • C.-H. Hsu
Conference paper
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

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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Copyright information

© Springer-Verlag Berlin Heidelberg 1993

Authors and Affiliations

  • C. H. Liu
    • 1
  • C.-H. Hsu
    • 2
  1. 1.NASA Langley Research CenterHamptonUSA
  2. 2.Vigyan, Inc.HamptonUSA

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