Abstract
An efficient finite—volume algorithm for three—dimensional Euler equations is presented. The spacial discretization is based on Van Leer's flux vector splitting. The flow field is analyzed by alternating sweeping in the spanwise direction and local Gauss-Seidel iteration on each vertical streamwise plane. Very large time step can be obtained since no factorization error is introduced and it leads to very rapid convergence rate. The memory resources are greatly saved since the Jacobians, the residual R and the δUn+1 are stored only in one iterating plane. Two internal transonic flows are calculated to show the efficiency and accuracy.
| Original language | English (US) |
|---|---|
| Title of host publication | 28th Aerospace Sciences Meeting, 1990 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| State | Published - 1990 |
| Externally published | Yes |
| Event | 28th Aerospace Sciences Meeting, 1990 - Reno, United States Duration: Jan 8 1990 → Jan 11 1990 |
Other
| Other | 28th Aerospace Sciences Meeting, 1990 |
|---|---|
| Country | United States |
| City | Reno |
| Period | 1/8/90 → 1/11/90 |
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ASJC Scopus subject areas
- Aerospace Engineering
Cite this
An efficient upwind relaxation–sweeping algorithm for three-dimensional euler equations. / Zha, GeCheng; Liu, Dao Zhi.
28th Aerospace Sciences Meeting, 1990. American Institute of Aeronautics and Astronautics Inc, AIAA, 1990. AIAA-90-0129.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - An efficient upwind relaxation–sweeping algorithm for three-dimensional euler equations
AU - Zha, GeCheng
AU - Liu, Dao Zhi
PY - 1990
Y1 - 1990
N2 - An efficient finite—volume algorithm for three—dimensional Euler equations is presented. The spacial discretization is based on Van Leer's flux vector splitting. The flow field is analyzed by alternating sweeping in the spanwise direction and local Gauss-Seidel iteration on each vertical streamwise plane. Very large time step can be obtained since no factorization error is introduced and it leads to very rapid convergence rate. The memory resources are greatly saved since the Jacobians, the residual R and the δUn+1 are stored only in one iterating plane. Two internal transonic flows are calculated to show the efficiency and accuracy.
AB - An efficient finite—volume algorithm for three—dimensional Euler equations is presented. The spacial discretization is based on Van Leer's flux vector splitting. The flow field is analyzed by alternating sweeping in the spanwise direction and local Gauss-Seidel iteration on each vertical streamwise plane. Very large time step can be obtained since no factorization error is introduced and it leads to very rapid convergence rate. The memory resources are greatly saved since the Jacobians, the residual R and the δUn+1 are stored only in one iterating plane. Two internal transonic flows are calculated to show the efficiency and accuracy.
UR - http://www.scopus.com/inward/record.url?scp=85003441340&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85003441340&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85003441340
BT - 28th Aerospace Sciences Meeting, 1990
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -