Application of HPCMP CREATE™-AV coffe for three-dimensional turbulent flow cases

J. Taylor Erwin; Ryan S. Glasb; Douglas L. Stefanski; Robert H. Nichols

Application of HPCMP CREATE^™-AV coffe for three-dimensional turbulent flow cases

J. Taylor Erwin, Ryan S. Glasb, Douglas L. Stefanski, Robert H. Nichols

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

16 Scopus citations

Abstract

HPCMP CREATE^™-AV Conservative Field Finite Element (COFFE) is applied to two specific three dimensional (3-D) turbulent flow cases as specified on the NASA Langley Research Center Turbulence Modeling Resource. These cases are subsonic flow over a 3-D bump in a channel and subsonic flow past a hemisphere cylinder at zero degrees angle of attack. Within COFFE, the Reynolds Averaged Navier-Stokes (RANS) equations tightly coupled with the Spalart-Allmaras turbulence model are discretized with the Streamwise Upwind/Petrov-Galerkin (SU/PG) finite element method. Computed results are validated against the NASA FUN3D Fully Unstructured Navier-Stokes code on identical computational meshes.

Original language	English
Title of host publication	54th AIAA Aerospace Sciences Meeting
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624103933
State	Published - 2016
Externally published	Yes
Event	54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States Duration: Jan 4 2016 → Jan 8 2016

Publication series

Name	54th AIAA Aerospace Sciences Meeting

Conference

Conference	54th AIAA Aerospace Sciences Meeting, 2016
Country/Territory	United States
City	San Diego
Period	01/4/16 → 01/8/16

Cite this

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title = "Application of HPCMP CREATE{\texttrademark}-AV coffe for three-dimensional turbulent flow cases",

abstract = "HPCMP CREATE{\texttrademark}-AV Conservative Field Finite Element (COFFE) is applied to two specific three dimensional (3-D) turbulent flow cases as specified on the NASA Langley Research Center Turbulence Modeling Resource. These cases are subsonic flow over a 3-D bump in a channel and subsonic flow past a hemisphere cylinder at zero degrees angle of attack. Within COFFE, the Reynolds Averaged Navier-Stokes (RANS) equations tightly coupled with the Spalart-Allmaras turbulence model are discretized with the Streamwise Upwind/Petrov-Galerkin (SU/PG) finite element method. Computed results are validated against the NASA FUN3D Fully Unstructured Navier-Stokes code on identical computational meshes.",

author = "Erwin, {J. Taylor} and Glasb, {Ryan S.} and Stefanski, {Douglas L.} and Nichols, {Robert H.}",

note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, All rights reserved.; 54th AIAA Aerospace Sciences Meeting, 2016 ; Conference date: 04-01-2016 Through 08-01-2016",

year = "2016",

language = "English",

isbn = "9781624103933",

series = "54th AIAA Aerospace Sciences Meeting",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "54th AIAA Aerospace Sciences Meeting",

}

Application of HPCMP CREATE^™-AV coffe for three-dimensional turbulent flow cases. / Erwin, J. Taylor; Glasb, Ryan S.; Stefanski, Douglas L. et al.
54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (54th AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Application of HPCMP CREATE™-AV coffe for three-dimensional turbulent flow cases

AU - Erwin, J. Taylor

AU - Glasb, Ryan S.

AU - Stefanski, Douglas L.

AU - Nichols, Robert H.

PY - 2016

Y1 - 2016

N2 - HPCMP CREATE™-AV Conservative Field Finite Element (COFFE) is applied to two specific three dimensional (3-D) turbulent flow cases as specified on the NASA Langley Research Center Turbulence Modeling Resource. These cases are subsonic flow over a 3-D bump in a channel and subsonic flow past a hemisphere cylinder at zero degrees angle of attack. Within COFFE, the Reynolds Averaged Navier-Stokes (RANS) equations tightly coupled with the Spalart-Allmaras turbulence model are discretized with the Streamwise Upwind/Petrov-Galerkin (SU/PG) finite element method. Computed results are validated against the NASA FUN3D Fully Unstructured Navier-Stokes code on identical computational meshes.

AB - HPCMP CREATE™-AV Conservative Field Finite Element (COFFE) is applied to two specific three dimensional (3-D) turbulent flow cases as specified on the NASA Langley Research Center Turbulence Modeling Resource. These cases are subsonic flow over a 3-D bump in a channel and subsonic flow past a hemisphere cylinder at zero degrees angle of attack. Within COFFE, the Reynolds Averaged Navier-Stokes (RANS) equations tightly coupled with the Spalart-Allmaras turbulence model are discretized with the Streamwise Upwind/Petrov-Galerkin (SU/PG) finite element method. Computed results are validated against the NASA FUN3D Fully Unstructured Navier-Stokes code on identical computational meshes.

UR - http://www.scopus.com/inward/record.url?scp=85007556890&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:85007556890

SN - 9781624103933

T3 - 54th AIAA Aerospace Sciences Meeting

BT - 54th AIAA Aerospace Sciences Meeting

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 54th AIAA Aerospace Sciences Meeting, 2016

Y2 - 4 January 2016 through 8 January 2016

ER -

Application of HPCMP CREATE^™-AV coffe for three-dimensional turbulent flow cases

Abstract

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