Test Data AC3-12

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Particle-laden swirling flow

Application Challenge AC3-12   © copyright ERCOFTAC 2013

Description of Test Case Experiments

For the detailed study of particle-laden, swirling two-phase flows, a vertical test section with downward flow was chosen (Figure 2). In order to allow good optical access, a simple pipe expansion was selected as test section. Such a configuration has the advantage that the inlet conditions can be measured easily, which is important for performing numerical calculations. The complete test rig consists of two flow circuits (Figure 1) for the primary (6) and secondary annular flows (5), respectively. A blower (1) with a variable flow rate supplies these two pipe systems via a T-junction and a throttle valve (2) is used to adjust the flow rate at the primary inlet. The mass flow rates through the primary and annular inlets were obtained from two orifice flow meters (3). The secondary flow circuit is split into four smaller pipes which are connected radially to the swirl generator. The upper part of the swirl generator is constructed as a settling chamber, and the air passes over a number of screens and then moves radially inward across the radial swirl vanes. The swirl intensity of the annular flow may be adjusted continuously by turning the swirl vanes in the radial swirl generator (8). The primary flow circuit is connected to a pipe passing straight through the centre of the swirl generator. The dust particles are injected into the primary flow above the swirl generator by a particle feeder (4) with a variable-speed motor. Above the particle feeder, a reservoir (7) for the dust particles is installed.

The inlet configuration and the dimensions of the test section are shown in Figure 1. The test section consists of a 1.5 m long Plexiglas tube with an inner diameter of 194 mm. The end of the test section is connected to a stagnation chamber (11). As a result, an annular type of central recirculation bubble was established in the upper part of the test section.

Figure 2: Overview of the swirl flow test facility.

The stagnation chamber is connected to a cyclone separator (13) and an additional paper filter to separate both the large dispersed phase particles and the seeding particles, which are used as tracers for measuring the gas velocity. These tracer particles are injected into both pipe systems before the swirl generator. To guarantee that the flow rate in the test section is independent of the pressure loss in the filter system, which may vary during the measurements, an additional blower (12) is used in connection with a bypass valve at the stagnation chamber (11).

Measurement Technique

Particle size and velocity measurements were performed at several cross- sections within the test section, including the inlet using a one- component PDA (phase-Doppler anemometer). Details on the configuration of the applied PDA-system can be found in Sommerfeld and Qiu (1991 and 1993). In order to allow measurements of all three velocity components (axial velocity u, radial velocity v, and tangential velocity w), the PDA system could be rotated and was mounted on a stepper-motor- controlled three-dimensional traversing system (Figure 1). The receiving optics was always mounted at an angle of 30( from the forward scattering direction. To avoid strong laser-beam deflections and a realignment of the receiving optics for every measuring point, the Plexiglas test section had several slits which were covered from the inside by 100 µm thick glass plates. This results in negligible beam distortion, especially when the radial and axial velocities are measured, where the receiving optics have to be mounted in such a way that the optical axis of the receiving optics is oblique to the walls of the test section. For each velocity component, different test sections with different slit locations were used, which allowed the appropriate installation of the PDA receiving optics and the measurement of particle size-velocity correlation for each velocity component.

In order to allow simultaneous measurements of gas and particle velocities, the flow was additionally seeded with small, spherical tracer particles (Ballotini, type 7000). This seeding was injected into both the primary and the annular jets far upstream the inlet to the test section. Since the size distribution of the particles ranges up to about 10 µm, a phase discrimination procedure was employed which ensured that only tracer particles up to a maximum of 4 µm are sampled for determining the gas velocity. This procedure resulted in a measured mean diameter of about 1.5 µm for the validated signals from the tracer particles. A detailed description of the phase discrimination procedure was given previously by Sommerfeld and Qiu (1991).

The particle mass flux was measured separately with the single-detector receiving system. The receiving optics was positioned 90° off-axis from the forward scattering direction in order to obtain an exact demarcation of the measuring volume. At each measuring point, the number of particles N traversing the control volume was counted within a certain time period (t, and the particle velocity was measured simultaneously. For these measurements the transient recorder was also operated in the sequential mode, which ensured a real-time data acquisition, at least for the particle concentrations considered. During the storage of the 400 events, an internal clock was used to determine the effective measuring time. The total particle mass flux is then obtained with the cross-section of the control volume Ac, which was calculated from the optical configuration:

${f_{p}={\frac {N{\overline {m}}_{p}}{\Delta tA_{c}}}}$

where ${\left.N\right.}$, ${\left.\Delta t\right.}$ and ${\overline {m_{p}}}$ are the counted number of particles, the total measuring time and the mean particle mass, respectively. The mean particle mass at a certain measuring location was calculated from the volume mean particle diameter obtained from the PDA size measurements. Due to the uncertainties in the determination of the cross-section of the control volume, the measured mass flux was corrected using the global mass balance. The total measured particle mass flow rate was obtained by integrating the mass flux profile at the inlet. In comparison with the global mass flow rate obtained by weighting the particles collected during a certain time period in the cyclone separator, a correction factor was determined and applied to the mass flux measurements at all other cross-sections. The integration of the measured and corrected mass flux profiles revealed that the error in the particle mass flow rate was in the range ( 20  % for the various profiles. This rather large error was caused mainly by the poor resolution of the measurements in the near-wall region, where the integration area is the largest in the circular cross-section of the pipe. Furthermore, the particle mass flux was separated to give the positive and negative fluxes, which gives additional information about the mass and number of particles having negative velocities. For this separation, the particle volume mean diameter for particles with only positive and negative axial velocity was determined from the PDA measurements.

Overview of Experimental Results

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Contributed by: Martin Sommerfeld — Martin-Luther-Universitat Halle-Wittenberg

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© copyright ERCOFTAC 2013