Sensitivity of an asymmetric, three-dimensional diffuser to inlet condition perturbations
Creators
- 1. Department of Aeronautics and Astronautics, Stanford University, 488 Escondido Mall, Building 500, Room 501W, Stanford, CA 94305 (United States)
- 2. Department of Mechanical Engineering, Stanford University, 488 Escondido Mall, Building 500, Room 501F, Stanford, CA 94305 (United States)
Description
Highlights: • Plasma actuators were used to manipulate secondary flow in the inlet of a diffuser. • Pulsed and steady forcing produce opposite effects on diffuser pressure recovery. • Planes of 2D PIV data were obtained from the midplane to the expanding sidewall. • Pulsed forcing produces a peak in Reynolds shear stress just upstream of separation. • Steady forcing leads to a differently-oriented large and unsteady separation bubble. - Abstract: The sensitivity of a three-dimensional, asymmetric diffuser to inlet condition perturbations was investigated using dielectric barrier discharge plasma actuators. Previous experimental and computational studies revealed the sensitivity of the separated flow in this diffuser to secondary flows in the inlet duct of the diffuser. By purposefully altering these secondary flows with highly tunable plasma actuators, the diffuser's pressure recovery could be both significantly improved and degraded. Two cases, one with pulsed forcing and another with continuous forcing, were selected for further study using 2D particle image velocimetry (PIV). PIV data were acquired in five streamwise-wall-normal planes. These measurements reveal that the relatively weak spanwise forcing introduced by the plasma actuators changes the size and orientation of the separation bubble. Pulsed forcing produces a strong peak in the Reynolds shear stress in the boundary layer upstream of separation. This significantly delays separation leading to a large increase in diffuser pressure recovery. In contrast, continuous plasma actuator forcing causes early separation on the diffuser sidewall, completely changing the separation geometry. This causes a larger and more unsteady separation bubble with higher reversed flow velocities which contribute to losses in the diffuser's pressure recovery
Availability note (English)
Available from http://dx.doi.org/10.1016/j.ijheatfluidflow.2014.04.008Additional details
Identifiers
- DOI
- 10.1016/j.ijheatfluidflow.2014.04.008;
- PII
- S0142-727X(14)00058-7;
Publishing Information
- Journal Title
- International Journal of Heat and Fluid Flow
- Journal Volume
- 49
- Journal Page Range
- p. 100-107
- ISSN
- 0142-727X
- CODEN
- IJHFD2
Conference
- Title
- 8. symposium on turbulence and shear flow phenomena
- Acronym
- TSFP8
- Dates
- 28-30 Aug 2013
- Place
- Poitiers (France)
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 47007755
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- ACTUATORS; ASYMMETRY; BOUNDARY LAYERS; BUBBLES; DIELECTRIC MATERIALS; DIFFUSERS; FLUID FLOW; PERTURBATION THEORY; PLASMA; REYNOLDS NUMBER; SENSITIVITY; THREE-DIMENSIONAL CALCULATIONS; TWO-DIMENSIONAL CALCULATIONS; WALLS
- Descriptors DEC
- DIMENSIONLESS NUMBERS; LAYERS; MATERIALS
Optional Information
- Copyright
- Copyright (c) 2014 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.