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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Date: 2014-04-29 15:57:45 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 Add to Reading List Source URL: aa.stanford.edu Download Document from Source Website File Size: 963,53 KB Share Document on Facebook

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