All Stories

  1. Numerical Investigation of the Linear and Nonlinear Transition Stages for a Sharp Cone at Mach 14

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  2. Numerical Investigation of Laminar-Turbulent Boundary-Layer Transition for an Ogive Geometry at Mach 7: Wind Tunnel and Flight Conditions

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  3. Numerical Investigation of Boundary-Layer Transition on a Sharp Cone at Mach 10

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  4. Controlled Transition Simulations on an Axisymmetric 8-Degree Compression Ramp at Mach 5

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Vasilis Tsakagiannis, Christoph Hader

  5. Delay of the Hot Streak Development for a Flared Cone at Mach 6

    Article • Journal of Spacecraft and Rockets, June 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  6. Numerical Investigations of the Linear Stability Regime for a Separation Bubble on an Axisymmetric Compression Ramp at Mach 5

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Vasilis Tsakagiannis, Christoph Hader

  7. Direct Numerical Simulation of Second-Mode Oblique Breakdown in a Mach 6 Sharp Cone Boundary Layer

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  8. Experimental Measurements of Hypersonic Boundary Layer Transition on the STORT Ogive Geometry

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

    Christoph Hader

  9. Numerical Investigation of the Linear and Nonlinear Transition Stages for a Sharp Cone at Mach 10

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

    Christoph Hader

  10. Numerical Investigations of the Linear and Nonlinear Transition Stages for a Hollow Cylinder Flare at Mach 5

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

    Christoph Hader, Vasilis Tsakagiannis

  11. Mori--Zwanzig Modal Decomposition: Applications and Analysis of Laminar-Turbulent Boundary Layer Transition

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

    Dr Daniel Livescu, Christoph Hader, Yifeng Tian

  12. Numerical Investigation of Hypersonic Boundary-Layer Transition for an Ogive Geometry

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

    Christoph Hader

  13. Numerical investigations of laminar-turbulent transition for a hollow cylinder flare at Mach 5

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

    Christoph Hader, Vasilis Tsakagiannis

  14. Transition Model for Second Mode and Crossflow Instabilities in Hypersonic Flow

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

    Christoph Hader

  15. Machine-Learning-Based Amplification Factor Transport Equation for Hypersonic Boundary-Layers

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  16. Numerical investigation of the nonlinear transition stages for a sharp cone at Mach 10

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  17. Direct Numerical Simulation for transitional flow using GPU acceleration

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader, Vasilis Tsakagiannis

  18. Flow control using steady blowing and suction strips in a Mach 6 Boundary Layer on a Flared Cone: “Natural” Transition

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  19. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Straight Cone at Mach 7

    Article • July 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  20. Direct Numerical Simulations of the Nonlinear Boundary Layer Transition Regime on a Flat Plate at Mach 6

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  21. Direct Numerical Simulations of Laminar-Turbulent Transition for Transonic Boundary Layers

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  22. Flow control using steady blowing and suction strips in a Mach 6 Boundary Layer on a Flared Cone

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  23. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a straight cone at Mach 5

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  24. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a slender cone

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  25. History and Progress of Boundary-Layer Transition on a Mach-6 Flared Cone

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Christoph Hader

  26. Towards simulating natural transition in hypersonic boundary layers via random inflow disturbances

    Article • Journal of Fluid Mechanics, May 2018, Cambridge University Press

    Christoph Hader

  27. Fundamental Resonance Breakdown for a Flared Cone at Mach 6

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

    Christoph Hader

  28. Laminar-Turbulent Transition on a Flared Cone at Mach 6

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

    Christoph Hader

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

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

    Christoph Brehm, Christoph Hader

  30. 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