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Floating shock fitting for three-dimensional inviscid supersonic flows - MaRDI portal

Floating shock fitting for three-dimensional inviscid supersonic flows (Q3968648)

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Floating shock fitting for three-dimensional inviscid supersonic flows
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    Floating shock fitting for three-dimensional inviscid supersonic flows (English)
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    1982
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    extending of two-dimensional floating shock-fitting computation technique to three dimensions
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    steady
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    aerodynamic bodies
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    contact surfaces
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    conventional marching procedures
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    subsonic axial Mach numbers
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    blunt- nosed wing/body combinations
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    various angles of attack
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