Browsing Aerospace Computational Design Laboratory: Technical Reports by Author "Modiano, David"

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    • Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow 

      Modiano, David (Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology, 1993-01)
      A solution method for the three-dimensional Euler equations is formulated and implemented. The solver uses an unstructured mesh of tetrahedral cells and performs adaptive refinement by mesh-point embedding to increase ...