Shock structure in separated nozzle flows (Q1932271)

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scientific article; zbMATH DE number 6126613
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English
Shock structure in separated nozzle flows
scientific article; zbMATH DE number 6126613

    Statements

    Shock structure in separated nozzle flows (English)
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    17 January 2013
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    rocket nozzle
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    Mach reflection
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    flow separation
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