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Einfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers

Einfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers

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This study investigates the effects of swirl on the supersonic wake of longitudinally-aligned axisymmetric afterbodies. The swirl was introduced upstream of the base corner by either spinning non-canted or non-spinning canted fins. Depending on the introduced swirl rate, both the experimental and numerical results show two distinctively different wake flow structures. The fluid-dynamic processes present in the rotating wakes and the resulting structural changes are analyzed in detail.

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Keywords

  • Drall
  • Mechanical engineering & materials
  • Numerical simulations
  • Numerische Simulationen
  • supersonic wake flow
  • swirl
  • Technology, engineering, agriculture
  • Überschallnachlauf
  • vortex breakdown
  • wind-tunnel measurements
  • Windkanalmessungen
  • Wirbelaufplatzen

Links

DOI: 10.5445/KSP/1000118606

Editions

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