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Interaction of separation and transition in laminar separation bubbles in a 3D boundary layer

Interaction of separation and transition in laminar separation bubbles in a 3D boundary layer
Interaction of separation and transition in laminar separation bubbles in a 3D boundary layer
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°. Instead, oblique waves with a propagation direction between 0° and -6° relative to the potential streamline trigger the strongest growth of background disturbances. Spatial linear stability theory (LST) was utilised to select the mosta mplified 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.
Hetsch, T.
3c399bce-3586-41e1-a93a-846b610c5ea6
Rist, U.
ce1897ad-3be7-4e55-b9db-9114d600f0da
Hetsch, T.
3c399bce-3586-41e1-a93a-846b610c5ea6
Rist, U.
ce1897ad-3be7-4e55-b9db-9114d600f0da

Hetsch, T. and Rist, U. (2004) Interaction of separation and transition in laminar separation bubbles in a 3D boundary layer. Research and Technology Organisation (RTO) Specialists Meeting on Enhancememnt of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation, Prague, Czech Republic. 03 - 07 Oct 2004.

Record type: Conference or Workshop Item (Paper)

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°. Instead, oblique waves with a propagation direction between 0° and -6° relative to the potential streamline trigger the strongest growth of background disturbances. Spatial linear stability theory (LST) was utilised to select the mosta mplified 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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More information

Published date: 2004
Venue - Dates: Research and Technology Organisation (RTO) Specialists Meeting on Enhancememnt of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation, Prague, Czech Republic, 2004-10-03 - 2004-10-07

Identifiers

Local EPrints ID: 23715
URI: http://eprints.soton.ac.uk/id/eprint/23715
PURE UUID: 8f4f592e-98dd-4a42-a283-828d5fdf992f

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Date deposited: 01 Jun 2006
Last modified: 11 Dec 2021 14:47

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Contributors

Author: T. Hetsch
Author: U. Rist

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