All Stories

  1. Additional Wind Tunnel Data for the Transonic LK6E2 Missile Airframe

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Erich Schülein

  2. Heat transfer amplifications in transitional shock-wave/boundary-layer interactions

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Erich Schülein

  3. Study of 2-D Shock-Wave / Turbulent Boundary Layer Interaction

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

    Dr. Erich Schülein, Mr Patrice Salif Richard Touré

  4. Experimental und numerical investigation of the aerodynamic characteristic of a generic transonic missile

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

    Dr. Erich Schülein

  5. A joint study on the starting limits of a generic supersonic inlet

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

    Dr. Erich Schülein

  6. High Frequency Free-Stream Disturbance Measurements in Hypersonic Wind Tunnels by Means of a Slender Wedge Probe

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

    Dr. Erich Schülein

  7. Simplified Model for Flow-Heating Effect on Wave Drag and Its Validation

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

    Dr. Erich Schülein

  8. Simplified model for flow-heating effect on wave drag of blunt bodies and its validation

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

    Dr. Erich Schülein

  9. Experimental Investigations on the Phantom Yaw Effect on a Maneuvering Slender Body

    Article • Journal of Spacecraft and Rockets, January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Erich Schülein

  10. Numerical investigation on the development of the Phantom Yaw Effect on a maneuvering missile

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

    Dr. Erich Schülein

  11. Effects of Laminar-Turbulent Transition on the Shock-Wave/Boundary-Layer Interaction

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

    Dr. Erich Schülein