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  1. Wingtip vortex structure in the near-field of swept-tapered wings

    Article • Physics of Fluids, September 2020, American Institute of Physics

    Shaun Skinner

  2. Methodology for Investigating the Effects of Wall Cooling on Hypersonic Boundary Layer Transition

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Shaun Skinner, Laura Paquin