Convergence Acceleration of an Upwind Least Squares Finite Difference based Meshless Solver

Author:

Sridar D.1,Balakrishnan N.1

Affiliation:

1. Indian Institute of Science, Bangalore 560 012, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference27 articles.

1. A perspective on a quarter century of CFD research

2. Euler calculations for multielement airfoils using Cartesian grids

3. An Accuracy Assessment of Cartesian-Mesh Approaches for the Euler Equations

4. Coirier, W. J. "An Adaptively-Refined Cartesian Cell Based Scheme for the Euler and Navier-Stokes Equations," Ph.D. thesis,Department of Aerospace Engineering, Universityof Michigan, Ann Arbor, MI,1994.

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