Interaction of Separation and Transition in Laminar Separation Bubbles in a 3D-Boundary Layer

Abstract

The influence of different disturbance combinations and increasing sweep on a family of pressure-induced laminar separation bubbles is studied systematically by means of direct numerical simulation (DNS). Three types of disturbance waves are tested against their potential to stimulate the growth of background disturbances of fundamental or subharmonic frequency. The focus is on 2D-disturbances, which are normally the most amplified disturbances in unswept separation bubbles. For the present 3D-base flows, they are found to lose their dominance for sweep angles larger than 10 to 15 degrees. Instead, oblique waves with a propagation direction between 0 degrees and -6 degrees relative to the potential streamline trigger the strongest growth of background disturbances. Spatial linear stability theory (LST) was utilised to select the most amplified disturbances for each sweep angle. LST turned out to be as reliable as in unswept laminar separation bubbles and its excellent agreement with DNS within the linear domain was not adversely affected by the sweep angle.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 2004
Accession Number
ADA442729

Entities

People

  • T. Hetsch
  • U. Rist

Organizations

  • University of Stuttgart

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Amplification
  • Base Flow
  • Boundaries
  • Boundary Layer
  • Boundary Layer Transition
  • Fluid Dynamics
  • Frequency
  • High Lift
  • High Lift Devices
  • Layers
  • Leading Edges
  • Pressure Gradients
  • Reynolds Number
  • Swept Wings
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Sensor Fusion and Tracking Systems.