All Stories

  1. Shock-Wave/Boundary-Layer Interaction in a Large-Aspect-Ratio Test Section

    Article • AIAA Journal, September 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mori Mani, Dr Richard K Scharnhorst, Miranda Pizzella

  2. Reynolds-Averaged Navier-Stokes Technology for Transonic Drag Prediction: A Boeing Perspective

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Richard K Scharnhorst, Dr. John A. Benek, Mori Mani, Miranda Pizzella

  3. Numerical Investigation of a Normal Shock Wave Boundary Layer Interaction in a 4.3 Aspect Ratio Test Section

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

    Dr Richard K Scharnhorst, Mori Mani, Miranda Pizzella

  4. Investigation of Shock Wave - Boundary Layer Interactions in a 3.57 Aspect Ratio Wind Tunnel

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

    Miranda Pizzella