All Stories

  1. An Immersed Boundary Method for Solving the Compressible Navier-Stokes Equations with Fluid-Structure Interaction

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm

  2. Noise generation mechanisms for a supersonic jet impinging on an inclined plate

    Article • Journal of Fluid Mechanics, May 2016, Cambridge University Press

    Christoph Brehm

  3. Open Rotor Computational Aeroacoustic Analysis with an Immersed Boundary Method

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm

  4. Noise Characteristics of a Four-Jet Impingement Device Inside a Broadband Engine Noise Simulator

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm

  5. A High-Order Immersed Interface Method for Compressible Flows

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm, Christoph Hader

  6. Numerical Investigation of transition delay for various controlled breakdown scenarios in a Mach 6 Boundary Layer using porous walls

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm, Christoph Hader

  7. The LAVA Computational Fluid Dynamics Solver

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm

  8. A Comparison of Higher-Order Shock Capturing Schemes Within the LAVA CFD Solver

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm

  9. Gradient Calculation Methods on Arbitrary Polyhedral Unstructured Meshes for Cell-Centered CFD Solvers

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Brehm