All Stories

  1. Evaluation of a Distributed Variable-Camber Trailing-Edge Flap System at Preliminary Aircraft Design Stage

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

    Florian Schueltke

  2. Implementation of an Airfoil Information Database for Usage in Conceptual Aircraft Wing Design Process

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

    Florian Schueltke

  3. Cross-flow effects regarding laminar flow control within conceptual aircraft design

    Article • Aircraft Engineering, July 2017, Emerald

    Florian Schueltke

  4. Variable Camber Impact on Aircraft Mission Planning

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

    Florian Schueltke

  5. Conceptual Wing Design Methodology for Aircraft with Hybrid Laminar Flow Control

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

    Florian Schueltke