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Magnetoaerodynamic boundary layer flow with pressure gradient and separation
Authors:A J Eggenberger and W F Hughes
Institution:(1) Carnegie Institute of Technology, Carnegie-Mellon University, Pittsburgh 13, Penn., USA;(2) Present address: University of South Carolina, Columbia, S.C., USA
Abstract:This study considers the large interaction parameter magnetoaerodynamic boundary layer associated with the free stream flow of a conducting fluid over an infinitely long circular insulator cylinder with the applied magnetic field normal to the distant free stream flow. The investigation is conducted in two parts; a theoretical solution of the associated boundary layer equations and a qualitative experimental investigation to allow visualization of flow separation caused by the magnetic field. The general integral formulation of Galerkin-Kantorovich-Dorodnitsyn is used to determine the boundary layer thickness, momentum thickness, displacement thickness, approximate separation point, and velocity profiles.
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