Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids (Q5942607)
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scientific article; zbMATH DE number 1643216
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids |
scientific article; zbMATH DE number 1643216 |
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Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids (English)
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2001
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The separation process between a supersonic rocket booster and an experimental supersonic airplane is simulated by means of overset unstructured grids. The airplane carries a stationary grid while the rocket booster is equipped with a moving grid. Numerical results are discussed.
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moving grid
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Chimera method
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