Numerical study on supersonic combustion with cavity-based fuel injection (Q1434579)
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scientific article; zbMATH DE number 2078421
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Numerical study on supersonic combustion with cavity-based fuel injection |
scientific article; zbMATH DE number 2078421 |
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Numerical study on supersonic combustion with cavity-based fuel injection (English)
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12 July 2004
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The authors investigate the effects of cavity on the hydrogen injection into a supersonic air flow. The cavity effect is discussed from a viewpoint of total pressure loss and combustion efficiency. The combustor with cavity is found to enhance mixing and combustion while increasing the pressure loss, compared with the case without cavity.
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supersonic air flow
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total pressure loss
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0.91828907
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0.8945119
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0.89215714
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0.8893117
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0.88572997
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0.8760042
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