Hypersonic simulations using open-source CFD and DSMC solvers

V. Casseau; T. J. Scanlon; B. John; D. R. Emerson; R. E. Brown

doi:10.1063/1.4967556

Hypersonic simulations using open-source CFD and DSMC solvers

V. Casseau, T. J. Scanlon, B. John, D. R. Emerson, R. E. Brown

Mechanical And Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

1 Citation (Scopus)

226 Downloads (Pure)

Abstract

Hypersonic hybrid hydrodynamic-molecular gas flow solvers are required to satisfy the two essential requirements of any high-speed reacting code, these being physical accuracy and computational efficiency. The James Weir Fluids Laboratory at the University of Strathclyde is currently developing an open-source hybrid code which will eventually reconcile the direct simulation Monte-Carlo method, making use of the OpenFOAM application called dsmcFoam, and the newly coded open-source two-temperature computational fluid dynamics solver named hy2Foam. In conjunction with employing the CVDV chemistry-vibration model in hy2Foam, novel use is made of the QK rates in a CFD solver. In this paper, further testing is performed, in particular with the CFD solver, to ensure its efficacy before considering more advanced test cases. The hy2Foam and dsmcFoam codes have shown to compare reasonably well, thus providing a useful basis for other codes to compare against.

Original language	English
Title of host publication	Proceedings of the 30th International Symposium on Rarefied Gas Dynamics
Editors	Henning Struchtrup, Andrew Ketsdever
Place of Publication	Melville, N.Y.
Number of pages	8
Volume	1786
DOIs	https://doi.org/10.1063/1.4967556
Publication status	Published - 16 Nov 2016
Event	30th International Symposium on Rarefied Gas Dynamics - University of Victoria, Victoria BC, Canada Duration: 10 Jul 2016 → 15 Jul 2016 https://conferences.uvic.ca/index.php/rgd/RGD30

Publication series

Name	AIP Conference Proceedings
Publisher	American Institute of Physics
Volume	1786
ISSN (Print)	0094-243X

Conference

Conference	30th International Symposium on Rarefied Gas Dynamics
Country/Territory	Canada
City	Victoria BC
Period	10/07/16 → 15/07/16
Internet address	https://conferences.uvic.ca/index.php/rgd/RGD30

Keywords

flow simulations
Testing procedures
chemically reactive flows
Monte Carlo method
hypersonic simulations
gas flow solvers
open-source hybrid code
OpenFOAM
navier stokes fourier equations

Access to Document

10.1063/1.4967556Licence: All rights reserved

Casseau-etal-SRGD2016-Hypersonic-simulations-using-open-source-CFD-and-DSMC-solversAccepted author manuscript, 512 KB

Cite this

@inproceedings{2d20c9ef5232488f9d2d479d2d7828bc,

title = "Hypersonic simulations using open-source CFD and DSMC solvers",

abstract = "Hypersonic hybrid hydrodynamic-molecular gas flow solvers are required to satisfy the two essential requirements of any high-speed reacting code, these being physical accuracy and computational efficiency. The James Weir Fluids Laboratory at the University of Strathclyde is currently developing an open-source hybrid code which will eventually reconcile the direct simulation Monte-Carlo method, making use of the OpenFOAM application called dsmcFoam, and the newly coded open-source two-temperature computational fluid dynamics solver named hy2Foam. In conjunction with employing the CVDV chemistry-vibration model in hy2Foam, novel use is made of the QK rates in a CFD solver. In this paper, further testing is performed, in particular with the CFD solver, to ensure its efficacy before considering more advanced test cases. The hy2Foam and dsmcFoam codes have shown to compare reasonably well, thus providing a useful basis for other codes to compare against.",

keywords = "flow simulations, Testing procedures, chemically reactive flows, Monte Carlo method, hypersonic simulations, gas flow solvers, open-source hybrid code, OpenFOAM, navier stokes fourier equations",

author = "V. Casseau and Scanlon, {T. J.} and B. John and Emerson, {D. R.} and Brown, {R. E.}",

note = "This article may be downloaded for personal use only. Any other use requires prior permission of the author and AIP Publishing. The following article appeared in Casseau, V., Scanlon, T. J., John, B., Emerson, D. R., & Brown, R. E. (2016). Hypersonic simulations using open-source CFD and DSMC solvers. In H. Struchtrup, & A. Ketsdever (Eds.), Proceedings of the 30th International Symposium on Rarefied Gas Dynamics . (Vol. 1786). [050006] (AIP Conference Proceedings; Vol. 1786). AIP Conference Proceedings. DOI: 10.1063/1.4967556) and may be found at http://dx.doi.org/10.1063/1.4967556; 30th International Symposium on Rarefied Gas Dynamics ; Conference date: 10-07-2016 Through 15-07-2016",

year = "2016",

month = nov,

day = "16",

doi = "10.1063/1.4967556",

language = "English",

isbn = "9780735414488",

volume = "1786",

series = "AIP Conference Proceedings",

publisher = "American Institute of Physics",

editor = "Henning Struchtrup and Andrew Ketsdever",

booktitle = "Proceedings of the 30th International Symposium on Rarefied Gas Dynamics",

url = "https://conferences.uvic.ca/index.php/rgd/RGD30",

}

Casseau, V, Scanlon, TJ, John, B, Emerson, DR & Brown, RE 2016, Hypersonic simulations using open-source CFD and DSMC solvers. in H Struchtrup & A Ketsdever (eds), Proceedings of the 30th International Symposium on Rarefied Gas Dynamics . vol. 1786, 050006, AIP Conference Proceedings, vol. 1786, Melville, N.Y., 30th International Symposium on Rarefied Gas Dynamics, Victoria BC, Canada, 10/07/16. https://doi.org/10.1063/1.4967556

Hypersonic simulations using open-source CFD and DSMC solvers. / Casseau, V.; Scanlon, T. J.; John, B.; Emerson, D. R.; Brown, R. E.

Proceedings of the 30th International Symposium on Rarefied Gas Dynamics . ed. / Henning Struchtrup; Andrew Ketsdever. Vol. 1786 Melville, N.Y., 2016. 050006 (AIP Conference Proceedings; Vol. 1786).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

TY - GEN

T1 - Hypersonic simulations using open-source CFD and DSMC solvers

AU - Casseau, V.

AU - Scanlon, T. J.

AU - John, B.

AU - Emerson, D. R.

AU - Brown, R. E.

N1 - This article may be downloaded for personal use only. Any other use requires prior permission of the author and AIP Publishing. The following article appeared in Casseau, V., Scanlon, T. J., John, B., Emerson, D. R., & Brown, R. E. (2016). Hypersonic simulations using open-source CFD and DSMC solvers. In H. Struchtrup, & A. Ketsdever (Eds.), Proceedings of the 30th International Symposium on Rarefied Gas Dynamics . (Vol. 1786). [050006] (AIP Conference Proceedings; Vol. 1786). AIP Conference Proceedings. DOI: 10.1063/1.4967556) and may be found at http://dx.doi.org/10.1063/1.4967556

PY - 2016/11/16

Y1 - 2016/11/16

N2 - Hypersonic hybrid hydrodynamic-molecular gas flow solvers are required to satisfy the two essential requirements of any high-speed reacting code, these being physical accuracy and computational efficiency. The James Weir Fluids Laboratory at the University of Strathclyde is currently developing an open-source hybrid code which will eventually reconcile the direct simulation Monte-Carlo method, making use of the OpenFOAM application called dsmcFoam, and the newly coded open-source two-temperature computational fluid dynamics solver named hy2Foam. In conjunction with employing the CVDV chemistry-vibration model in hy2Foam, novel use is made of the QK rates in a CFD solver. In this paper, further testing is performed, in particular with the CFD solver, to ensure its efficacy before considering more advanced test cases. The hy2Foam and dsmcFoam codes have shown to compare reasonably well, thus providing a useful basis for other codes to compare against.

AB - Hypersonic hybrid hydrodynamic-molecular gas flow solvers are required to satisfy the two essential requirements of any high-speed reacting code, these being physical accuracy and computational efficiency. The James Weir Fluids Laboratory at the University of Strathclyde is currently developing an open-source hybrid code which will eventually reconcile the direct simulation Monte-Carlo method, making use of the OpenFOAM application called dsmcFoam, and the newly coded open-source two-temperature computational fluid dynamics solver named hy2Foam. In conjunction with employing the CVDV chemistry-vibration model in hy2Foam, novel use is made of the QK rates in a CFD solver. In this paper, further testing is performed, in particular with the CFD solver, to ensure its efficacy before considering more advanced test cases. The hy2Foam and dsmcFoam codes have shown to compare reasonably well, thus providing a useful basis for other codes to compare against.

KW - flow simulations

KW - Testing procedures

KW - chemically reactive flows

KW - Monte Carlo method

KW - hypersonic simulations

KW - gas flow solvers

KW - open-source hybrid code

KW - OpenFOAM

KW - navier stokes fourier equations

UR - http://conferences.uvic.ca/index.php/rgd/RGD30/index

U2 - 10.1063/1.4967556

DO - 10.1063/1.4967556

M3 - Conference contribution book

SN - 9780735414488

VL - 1786

T3 - AIP Conference Proceedings

BT - Proceedings of the 30th International Symposium on Rarefied Gas Dynamics

A2 - Struchtrup, Henning

A2 - Ketsdever, Andrew

CY - Melville, N.Y.

T2 - 30th International Symposium on Rarefied Gas Dynamics

Y2 - 10 July 2016 through 15 July 2016

ER -

Hypersonic simulations using open-source CFD and DSMC solvers

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this