Manovski, Peter and Novara, Matteo and Schanz, Daniel and Geisler, Reinhard and Mohan, Nagendra Karthik Depuru and Schröder, Andreas (2017) 3D Lagrangian particle tracking of a transonic jet using four-pulse Shake-The-Box. 12th International Symposium on Particle Image Velocimetery, 2017-06-18 - 2017-06-22, Busan, Korea.
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Official URL: http://ispiv2017.org/
Abstract
Three-dimensional Lagrangian Particle Tracking (LPT) was performed on a transonic jet flow in air at Mach 0.84 generated by a round and chevron nozzle with an inner diameter (DDjj) of 15 mmmm. The ShakeThe-Box (STB) technique for multi-pulse data was employed to reconstruct particle tracks along the 4-pulse sequences and provided highly resolved accurate flow velocity and material acceleration data. The study of transonic jets has a long history both in the fields of fluid mechanics and aeroacoustics. To date there have only been a limited number of studies investigating these flow phenomena with volumetric measurement techniques. STB for time resolved applications (typically for flow speeds in air less than 30 m/s) is described in [S] and allows for accurate particle tracking of densely seeded (>O.OSppp) flows. Novara et al [3] showed that a short time sequence (or multi-pulse) implementation of STB was able to retrieve most particle tracks with dynamic velocity and acceleration ranges comparable to those obtained with STB in the time-resolved domain, and they stipulated the possibilities of measuring the material acceleration (and pressure) for high speed flows by means of multi-pulse acquisition systems. This experimental investigation shall serve to provide further validation and assessment in real experimental conditions. A multi-pulse setup with a combination of two dual-frarneacquisition systems was used to record tracer particle images of DEHS droplets (-1 µmm diameter) within a volume of 90x70x10 mmmm3 along the jet axial (xx) and two radial directions (yy) and (zz), respectively. The multi-pulse strategy described by (4] is applied here, where the use of two different states of polarization for the illumination sources is used to separate the pulses on the camera images [2]. The two imaging systems consisted each of four sCMOS PCO-Edge cameras and the digital resolution was -33.6 ppp /mmmm. An uneven pulse separation is employed to increase the velocity and acceleration dynamic ranges of the measurement. This allowed a maximum total particle shift of up to 100 px tobe measured. The seeding concentration for the experiment ranged from 0.02 to 0.05 pppppp. For each measurement configuration, a total of 40,000 4-pulse sequences were recorded at a sampling frequency of 10 H H H . The multi-pulse STB technique relies on the Iterative Particle Reconstruction technique (IPR, [6]) to reconstruct particle positions in a volume over a few recordings (typically four) and employs an iterative STB processing strategy to compensate for the lack of a long observation time [4].
| Item URL in elib: | https://elib.dlr.de/118516/ | ||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||
| Additional Information: | USB-Stick of Abstracts; ISPIV-130 | ||||||||||||||||||||||||||||
| Title: | 3D Lagrangian particle tracking of a transonic jet using four-pulse Shake-The-Box | ||||||||||||||||||||||||||||
| Authors: |
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| Date: | 2017 | ||||||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||
| Keywords: | Three-dimensional Lagrangian Particle Tracking (LPT), Shake-The-Box (STB) | ||||||||||||||||||||||||||||
| Event Title: | 12th International Symposium on Particle Image Velocimetery | ||||||||||||||||||||||||||||
| Event Location: | Busan, Korea | ||||||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||||||
| Event Start Date: | 18 June 2017 | ||||||||||||||||||||||||||||
| Event End Date: | 22 June 2017 | ||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Simulation and Validation (old) | ||||||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Experimental Methods, GO | ||||||||||||||||||||||||||||
| Deposited By: | Bachmann, Barbara | ||||||||||||||||||||||||||||
| Deposited On: | 26 Jan 2018 12:15 | ||||||||||||||||||||||||||||
| Last Modified: | 24 Apr 2024 20:22 |
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