All Stories

  1. A New Perspective on Battery-Electric Aviation, Part II: Conceptual Design of a 90-Seater

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

    Dr. ir. Roelof Vos

  2. Assessment of maximum range of battery-electric aircraft

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

    Dr. ir. Roelof Vos, Rob Wolleswinkel

  3. Aerodynamic Design of a Flying V Aircraft in Transonic Conditions

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

    Dr. ir. Roelof Vos

  4. Comparison of Future Aviation Fuels to Minimize the Climate Impact of Commercial Aircraft

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

    Pieter-Jan Proesmans, Dr. ir. Roelof Vos

  5. Conceptual design of a Flying-V aircraft family

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

    Wilco Oosterom, Dr. ir. Roelof Vos

  6. Selecting Technologies in Aircraft Conceptual Design Using Probabilistic Inversion

    Article • Journal of Aircraft, October 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. ir. Roelof Vos

  7. Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow

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

    georg eitelberg, Tomas Sinnige, prof. Leo Veldhuis, Dr. ir. Roelof Vos

  8. Aerodynamic Model Identification of the Flying V from Wind Tunnel Data

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

    Dr. ir. Roelof Vos

  9. Range Equation for Hybrid-Electric Aircraft with Constant Power Split

    Article • Journal of Aircraft, May 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. ir. Roelof Vos

  10. Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft

    Article • Journal of Aircraft, November 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Malcom Brown, Dr. ir. Roelof Vos

  11. The Effect of Maneuver Load Alleviation Strategies on Aircraft Performance Indicators

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

    Dr. ir. Roelof Vos, Andrea Mancini

  12. Aerodynamic Performance of an Aircraft Equipped with Horizontal Tail Mounted Propellers

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

    Dr. ir. Roelof Vos, prof. Leo Veldhuis

  13. Aerodynamic Interaction Between an Over-the-Wing Propeller and the Wing Boundary-Layer in Adverse Pressure Gradients

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

    Dr. ir. Roelof Vos, georg eitelberg, prof. Leo Veldhuis

  14. Automatically Generating the Technology Compatibility Matrix Using Graph Transformations

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

    Dr. ir. Roelof Vos

  15. Preliminary Sizing of a Hybrid-Electric Passenger Aircraft Featuring Over-the-Wing Distributed-Propulsion

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

    Dr. ir. Roelof Vos

  16. Conceptual Assessment of Hybrid Electric Aircraft with Distributed Propulsion and Boosted Turbofans

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

    prof. Leo Veldhuis, Dr. ir. Roelof Vos

  17. A Method for the Conceptual Design of Hybrid Electric Aircraft

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

    Dr. ir. Roelof Vos

  18. Effect of Propeller Installation on Performance Indicators of Regional Turboprop Aircraft

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

    Dr. ir. Roelof Vos, ir. Tom Schouten

  19. Aerodynamic Loads on an Aft-Mounted Propeller Induced by the Wing Wake

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

    Dr. ir. Roelof Vos, prof. Leo Veldhuis

  20. Formalizing Technology Descriptions for Selection During Conceptual Design

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

    Dr. ir. Roelof Vos

  21. The optimal cruise altitude of LNG-fuelled turbofan aircraft

    Article • Journal of Aerospace Operations, December 2017, IOS Press

    Dr. ir. Roelof Vos

  22. Handling Qualities Optimization in Aircraft Conceptual Design

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

    Dr. ir. Roelof Vos

  23. Aerodynamic Design of a Flying V Aircraft

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

    Dr. ir. Roelof Vos

  24. Cruise Performance Optimization of the Airbus A320 through Flap Morphing

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

    Dr. ir. Roelof Vos, Martin Orlita

  25. Semi-Analytical Composite Oval Fuselage Weight Estimation

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

    Dr. ir. Roelof Vos

  26. Modeling the Propeller Slipstream Effect on Lift and Pitching Moment

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

    Dr. ir. Roelof Vos

  27. Conceptual Design of Swept-Wing Root Airfoils

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

    Dr. ir. Roelof Vos

  28. Development of a Wave Drag Prediction Method for the Conceptual Design Phase

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

    Dr. ir. Roelof Vos

  29. Assessing the Effect of Decreased Longitudinal Stability on Aircraft Size and Performance

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

    Dr. ir. Roelof Vos

  30. Effect of Wing Loading and Fuel Type on Optimal Cruise Altitude for Civil Aircraft

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

    Dr. ir. Roelof Vos

  31. A Practical Method for Uncertainty Analysis in the Aircraft Conceptual Design Phase

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

    Dr. ir. Roelof Vos

  32. Knowledge-Based Engineering Approach to the Finite Element Analysis of the Oval Fuselage Concept

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

    Dr. ir. Roelof Vos

  33. Analysis of a Ground-Based Magnetic Propulsion System

    Article • Journal of Aircraft, May 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. ir. Roelof Vos, Catherine Eeckels

  34. A Semi-Analytical Weight Estimation Method for Oval Fuselages in Conventional and Novel Aircraft

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

    Dr. ir. Roelof Vos