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Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow - MaRDI portal

Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow (Q5304080)

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scientific article; zbMATH DE number 5683892
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Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow
scientific article; zbMATH DE number 5683892

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    Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow (English)
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    18 March 2010
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    chemically reactive flow
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    chromium
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    drag reduction
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    enthalpy
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    flow visualisation
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    hypersonic flow
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    oxygen
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    shock waves
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    thermochemistry
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