Giglmaier, Marcus and Quaatz, Jan Frederik and Gawehn, Thomas and Gülhan, Ali and Adams, N. A. (2014) Numerical and experimental investigations of pseudo-shock systems in a planar nozzle: impact of bypass mass flow due to narrow gaps. Shock Waves, 24 (2), pp. 139-156. Springer. doi: 10.1007/s00193-013-0475-2. ISSN 0938-1287.
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Official URL: http://dx.doi.org/10.1007/s00193-013-0475-2
Abstract
During previous investigations on pseudo-shock systems, we have observed reproducible differences between measurement and simulations for the pressure distribution as well as for size and shape of the pseudo-shock system. A systematic analysis of the deviations leads to the conclusion that small gaps of Δz=O(10 −4 ) m between quartz glass side walls and metal contour of the test section are responsible for this mismatch. This paper describes a targeted experimental and numerical study of the bypass mass flow within these gaps and its interaction with the main flow. In detail, we analyze how the pressure distribution within the channel as well as the size, shape and oscillation of the pseudo-shock system are affected by the gap size. Numerical simulations are performed to display the flow inside the gaps and to reproduce and explain the experimental results. Numerical and experimental schlieren images of the pseudo-shock system are in good agreement and show that especially the structure of the primary shock is significantly altered by the presence of small gaps. Extensive unsteady flow simulations of the geometry with gaps reveal that the shear layer between subsonic gap flow and supersonic core flow is subject to a Kelvin–Helmholtz instability resulting in small pressure fluctuations. This leads to a shock oscillation with a frequency of f=O(10 5 )s −1 . The corresponding time scale τ (s) is 16 times higher than the characteristic time scale τ δ =δ/U ∞ of the boundary layer given by the ratio of the boundary layer thickness δ directly ahead of the shock and the undisturbed free stream velocity U ∞ . To assess the reliability of our numerical investigations, the paper includes a grid study as well as an extensive comparison of several RANS turbulence models and their impact on the predicted shape of pseudo-shock systems.
| Item URL in elib: | https://elib.dlr.de/88387/ | ||||||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||||||
| Additional Information: | Online erschienen am 19. Oktober 2013 | ||||||||||||||||||||||||
| Title: | Numerical and experimental investigations of pseudo-shock systems in a planar nozzle: impact of bypass mass flow due to narrow gaps | ||||||||||||||||||||||||
| Authors: |
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| Date: | 1 March 2014 | ||||||||||||||||||||||||
| Journal or Publication Title: | Shock Waves | ||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||
| Volume: | 24 | ||||||||||||||||||||||||
| DOI: | 10.1007/s00193-013-0475-2 | ||||||||||||||||||||||||
| Page Range: | pp. 139-156 | ||||||||||||||||||||||||
| Publisher: | Springer | ||||||||||||||||||||||||
| ISSN: | 0938-1287 | ||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||
| Keywords: | Pseudo-shock system Shock oscillation CFD Shock wave–turbulent boundary layer interaction | ||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||
| HGF - Program: | Space | ||||||||||||||||||||||||
| HGF - Program Themes: | Space Transportation | ||||||||||||||||||||||||
| DLR - Research area: | Raumfahrt | ||||||||||||||||||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||||||||||||||||||
| DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old) | ||||||||||||||||||||||||
| Location: | Köln-Porz | ||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology | ||||||||||||||||||||||||
| Deposited By: | Gawehn, Dr.-Ing. Thomas | ||||||||||||||||||||||||
| Deposited On: | 25 Mar 2014 08:52 | ||||||||||||||||||||||||
| Last Modified: | 13 Dec 2022 14:29 |
Available Versions of this Item
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Numerical and experimental investigations of pseudo-shock
systems in a planar nozzle: impact of bypass mass flow
due to narrow gaps. (deposited 14 Jan 2014 08:46)
- Numerical and experimental investigations of pseudo-shock systems in a planar nozzle: impact of bypass mass flow due to narrow gaps. (deposited 25 Mar 2014 08:52) [Currently Displayed]
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