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10.57647/j.jtap.2024.1805.70

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Assessment of a compressible lattice Boltzmann method in analyzing shock wave/boundary layer interaction in a supersonic inlet

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Turbulent boundary layer/shock wave interaction in a nozzle using a compressible lattice Boltzmann method

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10.57647/j.jtap.2025.1905.49

Requires Subscription PDF downloads: 104