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Visual hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets

Visual hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets
Visual hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets
Three-dimensional shock structures produced by Mach 1.45 supersonic bevelled jets were digitally reconstructed based on schlieren photography and a voxel-based visual hull technique. By taking advantage of the strong edge features commonly found in schlieren images of shock waves, the proposed technique demonstrates the possibility of performing shock wave reconstruction in supersonic jet applications without prior knowledge of the global density or velocity field. Semi-synthetic camera parameters were introduced as a method to circumvent camera calibration issues faced in the reconstruction procedure. This is key to achieving accurate and high-resolution reconstructed shock waves for both axisymmetric and asymmetric test cases with an average of 2.5% error when validated against raw schlieren images. When applied to bevelled jets with non-uniform nozzle exit geometries, an additional assumption was made to address the problem of schlieren line-of-sight blockage by the non-conventional nozzle, and reconstruction errors were found to be larger near regions of poorer shock wave contrast. Current results indicate that the technique is robust and fast during image calibration and processing, with accuracy of reconstructed shock waves in both conventional and non-conventional nozzles strongly dependent on shock wave contrast. Compared to existing techniques that can be used to reconstruct 3D shock structures, the proposed technique has the advantage of being totally non-intrusive as compared to point or particle-based measurements, requires significantly less computation than tomographic methods, offers high resolution reconstruction even with limited camera resolution and projected schlieren views, and is easy and cost effective to implement.
0894-1777
458-473
Lim, Desmond
82a7e7e8-2ade-44f8-a342-a99c2b9339c4
New, T.H.
f35405df-ad65-4b96-9d6b-06afebdd43a8
Mariani, R
dce93d9c-b1ec-46c7-90a4-27f01eaf3b5d
Cui, Y D
432f25aa-b68a-4cc7-b6a7-98f93e044e41
Lim, Desmond
82a7e7e8-2ade-44f8-a342-a99c2b9339c4
New, T.H.
f35405df-ad65-4b96-9d6b-06afebdd43a8
Mariani, R
dce93d9c-b1ec-46c7-90a4-27f01eaf3b5d
Cui, Y D
432f25aa-b68a-4cc7-b6a7-98f93e044e41

Lim, Desmond, New, T.H., Mariani, R and Cui, Y D (2018) Visual hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets. Experimental Thermal and Fluid Science, 99, 458-473. (doi:10.1016/j.expthermflusci.2018.08.022).

Record type: Article

Abstract

Three-dimensional shock structures produced by Mach 1.45 supersonic bevelled jets were digitally reconstructed based on schlieren photography and a voxel-based visual hull technique. By taking advantage of the strong edge features commonly found in schlieren images of shock waves, the proposed technique demonstrates the possibility of performing shock wave reconstruction in supersonic jet applications without prior knowledge of the global density or velocity field. Semi-synthetic camera parameters were introduced as a method to circumvent camera calibration issues faced in the reconstruction procedure. This is key to achieving accurate and high-resolution reconstructed shock waves for both axisymmetric and asymmetric test cases with an average of 2.5% error when validated against raw schlieren images. When applied to bevelled jets with non-uniform nozzle exit geometries, an additional assumption was made to address the problem of schlieren line-of-sight blockage by the non-conventional nozzle, and reconstruction errors were found to be larger near regions of poorer shock wave contrast. Current results indicate that the technique is robust and fast during image calibration and processing, with accuracy of reconstructed shock waves in both conventional and non-conventional nozzles strongly dependent on shock wave contrast. Compared to existing techniques that can be used to reconstruct 3D shock structures, the proposed technique has the advantage of being totally non-intrusive as compared to point or particle-based measurements, requires significantly less computation than tomographic methods, offers high resolution reconstruction even with limited camera resolution and projected schlieren views, and is easy and cost effective to implement.

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More information

Accepted/In Press date: 17 August 2018
e-pub ahead of print date: 18 August 2018
Published date: 1 December 2018
Additional Information: © 2018 Elsevier Inc. All rights reserved

Identifiers

Local EPrints ID: 469264
URI: http://eprints.soton.ac.uk/id/eprint/469264
ISSN: 0894-1777
PURE UUID: 902f779c-5196-405c-95fe-84894b302eb5
ORCID for Desmond Lim: ORCID iD orcid.org/0000-0001-6191-6803

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Date deposited: 12 Sep 2022 16:34
Last modified: 16 Mar 2024 21:04

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Contributors

Author: Desmond Lim ORCID iD
Author: T.H. New
Author: R Mariani
Author: Y D Cui

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