The studies of finite supercavitating airfoil (Q1094228)
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scientific article; zbMATH DE number 4024974
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | The studies of finite supercavitating airfoil |
scientific article; zbMATH DE number 4024974 |
Statements
The studies of finite supercavitating airfoil (English)
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1986
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The author has considered the flow past an aerofoil above which artificial cavitated low pressure region is built, with high speed airflow jet in the aerofoil. Two assumptions are made. Cavity pressure of whole cavity is uniform. About the wall jet, it is assumed that the increase of flow velocity can be neglected and is caused by the low pressure of low pressure eddy region. Using the generalized Blasius's theorem and conformal transformation, the formula for the lift and thrust are derived.
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flow past an aerofoil
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artificial cavitated low pressure region
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high speed airflow jet
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wall jet
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generalized Blasius's theorem
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conformal transformation
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0.88474566
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0.86088777
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0.85484076
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0.84978676
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0.8482665
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0.8469057
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0.8456437
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