Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers (Q1973769)
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scientific article; zbMATH DE number 1441146
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers |
scientific article; zbMATH DE number 1441146 |
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Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers (English)
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8 May 2000
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supersonic transport configuration
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aerodynamic shape optimization
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Euler equations
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control theory
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domain decomposition approach
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optimized communication schedule
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message passing interface
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0.8679227
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0.86217517
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0.85906327
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