development and validation of a density-based implicit...
TRANSCRIPT
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Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
JaeHeung Gill1, ByoungYun Kim1, JiHong Kim2, HoonBum Shin2, SungKi Jung2 and KyuHong Kim3
1 NEXTFoam Co., Ltd.
2 Korea Aerospace Indutries, LTD.
3 Seoul National University
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3Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 3: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/3.jpg)
4Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 4: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/4.jpg)
5Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Background
Based on DensityBasedTurbo by Oliver Borm– Density Based Coupled Algorithm– Explicit Time Integration– Godunov Type Flux Schemes– Multi-Dimensional Slope Limiter– Local Time Stepping– Steady & Transient Solvers
We have focused on steady state solver– Implementation of implicit time integration– Implementation of far-field boundary condition
● Utilizing riemann invariants
![Page 5: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/5.jpg)
6Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 6: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/6.jpg)
7Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Implicit Finite Volume Discretization
Favre-Averaged Navier-Stokes Equations in Integral Form
∫V∂W∂ t
dV +∮S ( F c− F v ) dS=0
W=[ρρ UρE ] F c=[
(ρU ) f⋅n
(ρ U⊗U + p I ) f⋅n
(ρH U ) f⋅n]
F v=[0τ f⋅n
( τ⋅n ) f⋅n+(ραeff ∇ h ) f⋅n+{(μ+μ tσk )∇ k } f⋅n]
![Page 7: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/7.jpg)
8Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Implicit Finite Volume Discretization
Spatial Discretization
V i
∂W i
∂ t+ ∑
j∈N (i)( F c , ij− F v , ij ) S ij=0
i
j
j
j
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9Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Implicit Finite Volume Discretization
Time Integration
– Explicit
– Implicit ( Backward Euler)
V i
Δ t i(W i
n+1−W in)+ ∑
j∈N (i)( F c , ij
n − F v ,ijn ) S ij=0
V i
Δ t i(W i
n+1−W i
n)+ ∑j∈N (i)
( F c , ijn+1− F v , ij
n+1)S ij=0
![Page 9: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/9.jpg)
10Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Implicit Finite Volume Discretization
Linearizing Flux Vector– Linearizing both convective and viscous fluxes using Taylor's series expansion.
Result in
where
F ijn+1≈ F ij
n+( ∂ F∂W )ijΔ W ijn
V i
Δ t iΔ W i
n+ ∑j∈N (i )
( Ac ,ij−Av ,ij )Δ W ijn S ij=−Res i
n
Δ W in=W i
n+1−W i
n
Ac=∂ F c
∂W: Convective Flux Jacobian
Av=∂ F v
∂ W: Viscous Flux Jacobian
![Page 10: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/10.jpg)
11Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 11: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/11.jpg)
12Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
Evaluation of Flux Jacobian– Steger-Warming's Flux Vector Splitting for Convective Flux– Thin Shear Layer Approximation(TSL) for Viscous Flux
V i
Δ t iΔ W i
n+ ∑
j∈N (i)(Ac ,i
+Av ,i
∗)Δ W i
n S ij
+ ∑j∈N (i)
(Ac , j−−Av , j
∗)ΔW j
n S ij=−Resin
![Page 12: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/12.jpg)
13Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
Split off-diagonal term into lower(owner) and upper(neighbor) part
– Block matrix system
V i
Δ t iΔ W i
n+ ∑
j∈N (i)(Ac ,i
+Av ,i
∗)ΔW i
n S ij
+ ∑j∈L (i)
( Ac , j−−Av , j
∗)Δ W j
n S ij
+ ∑j∈U (i )
(Ac , j−−Av , j
∗)Δ W j
n S ij=−Resin
(D+L+U )ΔW n=−Rn
![Page 13: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/13.jpg)
14Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
Block Matrix Example
1
4
56
3
2
0
13
10
7
1211
8
9
(D0 U1 0 0 0 0 0 0 U 8 0 0 0 0 0L0 D1 0 0 0 0 0 0 0 U 9 0 0 0 00 0 D2 U 3 0 0 0 0 0 U 9 0 0 0 0
0 0 L2 D3 0 0 0 0 0 0 0 U 11 0 00 0 0 0 D4 U 5 0 0 0 0 0 U 11 0 00 0 0 0 L4 D5 0 0 0 0 U 10 0 0 00 0 0 0 0 0 D6 U 7 0 0 U 10 0 0 0
0 0 0 0 0 0 L6 D 7 U 8 0 0 0 0 0L0 0 0 0 0 0 0 L7 D 8 0 0 0 0 U 13
0 L1 L2 0 0 0 0 0 0 D9 0 0 0 U 13
0 0 0 0 0 L5 L6 0 0 0 D10 0 U 12 00 0 0 L3 L4 0 0 0 0 0 0 D11 U 12 00 0 0 0 0 0 0 0 0 0 L10 L11 D12 U 13
0 0 0 0 0 0 0 0 L8 L9 0 0 L12 D13
)D+L+U
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15Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
Approximate Factorization
– Factorization error
(D+L)D−1(D+U )ΔW n=−Rn+LD−1U ΔW n
ο(Δ t2) if Δ t≪Δ xο(Δ t) if Δ t≫Δ x
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16Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
Invert the matrix in two steps– Forward sweep
(D+L)ΔW∗=−Rn
(D0 0 0 0 0 0 0 0 0 0 0 0 0 0L0 D1 0 0 0 0 0 0 0 0 0 0 0 00 0 D2 0 0 0 0 0 0 0 0 0 0 00 0 L2 D3 0 0 0 0 0 0 0 0 0 00 0 0 0 D4 0 0 0 0 0 0 0 0 00 0 0 0 L4 D5 0 0 0 0 0 0 0 00 0 0 0 0 0 D6 0 0 0 0 0 0 00 0 0 0 0 0 L6 D7 0 0 0 0 0 0L0 0 0 0 0 0 0 L7 D8 0 0 0 0 00 L1 L2 0 0 0 0 0 0 D9 0 0 0 00 0 0 0 0 L5 L6 0 0 0 D10 0 0 00 0 0 L3 L4 0 0 0 0 0 0 D11 0 00 0 0 0 0 0 0 0 0 0 L10 L11 D12 00 0 0 0 0 0 0 0 L8 L9 0 0 L12 D13
)(ΔW 0
∗
ΔW 1∗
ΔW 2∗
ΔW 3∗
ΔW 4∗
ΔW 5∗
ΔW 6∗
ΔW 7∗
ΔW 8∗
ΔW 9∗
ΔW 10∗
ΔW 11∗
ΔW 12∗
ΔW 13∗
) = −[Rn ]
![Page 16: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/16.jpg)
17Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Lower-Upper Symmetric Gauss-Seidel(LU-SGS) Algorithm
– Backward sweep
(D+U )ΔW n=DΔW∗
(D0 U 1 0 0 0 0 0 0 U 8 0 0 0 0 00 D1 0 0 0 0 0 0 0 U 9 0 0 0 0
0 0 D2 U 3 0 0 0 0 0 U 9 0 0 0 00 0 0 D3 0 0 0 0 0 0 0 U 11 0 00 0 0 0 D4 U 5 0 0 0 0 0 U 11 0 00 0 0 0 0 D5 0 0 0 0 U 10 0 0 0
0 0 0 0 0 0 D6 U 7 0 0 U 10 0 0 00 0 0 0 0 0 0 D7 U 8 0 0 0 0 00 0 0 0 0 0 0 0 D8 0 0 0 0 U 13
0 0 0 0 0 0 0 0 0 D9 0 0 0 U 13
0 0 0 0 0 0 0 0 0 0 D10 0 U 12 00 0 0 0 0 0 0 0 0 0 0 D11 U 12 00 0 0 0 0 0 0 0 0 0 0 0 D12 U 13
0 0 0 0 0 0 0 0 0 0 0 0 0 D13
)(ΔW 0
n
ΔW 1n
ΔW 2n
ΔW 3n
ΔW 4n
ΔW 5n
ΔW 6n
ΔW 7n
ΔW 8n
ΔW 9n
ΔW 10n
ΔW 11n
ΔW 12n
ΔW 13n
) = [D ΔW∗]
![Page 17: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/17.jpg)
18Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 18: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/18.jpg)
19Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Inviscid Flow(2D)
Transonic Flow over a Bump in Channel– 65 X 17 grid
– M∞ = 0.675
From Ni, 1982
Current
Residual history
Current(maxCo = 500)
Explicit(maxCo = 2)
![Page 19: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/19.jpg)
20Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Inviscid Flow(2D)
Oblique Shock Reflection on a Plane Wall– Uniform triangular grid
– M∞ = 2.9
commercial
![Page 20: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/20.jpg)
21Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(2D)
Transonic Flow Over RAE2822 Airfoil– 36,000 cells Hybrid(quad + tri) grid
– M∞ = 0.675
– komegaSST turbulence model
0 0.2 0.4 0.6 0.8 1
-1.5
-1
-0.5
0
0.5
1
1.5EXP
OpenFOAM
Commercial
WIND V5
WIND v1
NPARC
x/c
-Cp
![Page 21: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/21.jpg)
22Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow over ONERA M6 Wing– M
∞ = 0.8395, p
∞=315980pa, T
∞=255.56K
– AoA = 3.06– Hex(NASA) and hybrid mesh
OpenFOAMOpenFOAM
Commercial code Commercial code
![Page 22: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/22.jpg)
23Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow over ONERA M6 Wing
![Page 23: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/23.jpg)
24Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow over ONERA M6 Wing
0 0.2 0.4 0.6 0.8 1
-1
-0.5
0
0.5
1
1.5y/b=0.2
Wind
OpenFOAM
x/l
-Cp
0 0.2 0.4 0.6 0.8 1
-1
-0.5
0
0.5
1
1.5y/b=0.44
Wind
OpenFOAM
x/l
-Cp
![Page 24: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/24.jpg)
25Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow over ONERA M6 Wing
0 0.2 0.4 0.6 0.8 1
-1
-0.5
0
0.5
1
1.5y/b=0.65
Wind
OpenFOAM
x/l
-Cp
0 0.2 0.4 0.6 0.8 1
-1
-0.5
0
0.5
1
1.5y/b=0.9
Wind
OpenFOAM
x/l
-Cp
![Page 25: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/25.jpg)
26Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow around DLR F4 Wing-Body– M
∞ = 0.75, p
∞=116577pa, T
∞=300K
– AoA = 0.49– Hybrid mesh from AIAA DPW II ( 5,200,000 cells )
OpenFOAM
Commercial Code
![Page 26: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/26.jpg)
27Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow around DLR F4 Wing-Body
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
-1
-0.5
0
0.5
1
1.5y/b=0.239
Wind TunnelOF-ImplicitCommercial
x/c
-Cp
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
-1
-0.5
0
0.5
1
1.5y/b=0.377
Wind TunnelOF-ImplicitCommercial
x/c
-Cp
![Page 27: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/27.jpg)
28Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Results – Viscous Turbulent Flow(3D)
Transonic Flow around DLR F4 Wing-Body
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
-1
-0.5
0
0.5
1
1.5y/b=0.514
Wind TunnelOF-ImplicitCommercial
x/c
-Cp
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
-1
-0.5
0
0.5
1
1.5y/b=0.847
Wind TunnelOF-ImplicitCommercial
x/c
-Cp
![Page 28: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/28.jpg)
29Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Outline
1. Background
2. Implicit Finite Volume Discretization
3. LU-SGS Algorithm
4. Results
5. Concluding Remarks
![Page 29: Development and Validation of a Density-Based Implicit ...nextfoam.co.kr/proc/DownloadProc.php?fName=... · Results – Viscous Turbulent Flow(3D) Transonic Flow over ONERA M6 Wing](https://reader034.vdocument.in/reader034/viewer/2022042622/5f859a0db7c0a97dce497666/html5/thumbnails/29.jpg)
30Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm
Concluding Remarks
Summary– Implicit LU-SGS algorithm and new boundary condition have been
implemented – The numerical results obtained indicate that implicit algorithm leads to an
increase in performance over the explicit counter part– Solution was comparable to commercial code
Future works– More efficient version of LU-SGS– Low mach number preconditioning– Multigrid
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Development and Validation of a Density-Based Implicit Solver Using LU-SGS Algorithm 31
Thank you …Thank you …
… for your attention!