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Fluid dynamics / Airspeed / Piping / Laminar-turbulent transition / Hypersonic speed / Mach number / Reynolds number / Swept wing / Compressibility / Aerospace engineering / Aerodynamics / Fluid mechanics


Crossflow Instability in Three-Dimensional Hypersonic Boundary Layers Wade M. Spurlock, Sanjiva K. Lele Department of Aeronautics and Astronautics Overview Motivation
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Document Date: 2014-04-29 15:57:45

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File Size: 963,53 KB

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Cascade Technologies / /

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Stanford University / /

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coordinate systems / /

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Unsteady Flow Physics and Aeroacoustics Lab / Department of Aeronautics and Astronautics / Japan Society for Aeronautical and Space Sciences / Stanford University / Sanjiva K. Lele Department of Aeronautics / /

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Viktor Ya / Blackbird / Boris V. Smorodsky / John Schmisseur / Sergey A. Gaponov / Kenneth J. Franko / /

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Author / Program Manager / /

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Falcon / swept wing / /

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Journal of Computational Physics / /

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Stanford University / /

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DNS / /

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