Application of a partitioned field approach to transient aerothermal problems in rocket nozzles (Q1643695)
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scientific article; zbMATH DE number 6891034
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Application of a partitioned field approach to transient aerothermal problems in rocket nozzles |
scientific article; zbMATH DE number 6891034 |
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Application of a partitioned field approach to transient aerothermal problems in rocket nozzles (English)
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19 June 2018
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aerothermoelasticity
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partitioned field approach
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axisymmetric shells
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rocket nozzles
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