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About contributions to aerodynamic shape optimization
solved using an efficient parallel Newton-Krylov-Schur strategy. A gradient-based and mesh equations in a sequential approach. The flow adjoint
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2009 |
| Pages: | 164 |
| Language: | English |
| File Size: | 7.01 |
| Format: | |
| Price: | FREE |
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