All Stories

  1. Creep behaviour of Ti-6Al-4V produced by SLM

    Article • January 2019, American Institute of Physics

    ir Sjoerd O van der Veen

  2. Measurement and modelling of residual stress in wire-feed additively manufactured titanium

    Article • Materials Science and Technology, October 2018, Taylor & Francis

    Professor Michael Fitzpatrick, ir Sjoerd O van der Veen

  3. Impact of forming process on static, fatigue and damage tolerance properties

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

    ir Sjoerd O van der Veen

  4. Predicting the paths of fatigue cracks in alloys with anisotropic crack resistance

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

    ir Sjoerd O van der Veen, Dr.ir. René C Alderliesten

  5. Residual Fatigue Properties of a 2024-T351 Aluminium Alloy from the Teardown of AIRBUS A320 Wing Panels after Service

    Article • Advanced Materials Research, March 2014, Trans Tech Publications

    ir Sjoerd O van der Veen

  6. Novel Aerospace Architectures Made Possible by Forming Simulation

    Article • Key Engineering Materials, June 2013, Trans Tech Publications

    ir Sjoerd O van der Veen

  7. AK-ILS: An Active learning method based on Kriging for the Inspection of Large Surfaces

    Article • Precision Engineering, January 2013, Elsevier

    ir Sjoerd O van der Veen

  8. Tailoring Static Strength Performance of Metallic Stiffened Panels by Selective Local Sub-Stiffening

    Article • May 2006, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen, Mustafa Ozakca

  9. Post-Buckling Failure of Welded Aluminum Panels

    Article • May 2006, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen

  10. Stiffened Panels in Compression: Redirecting Loads Toward High-Strength Stiffeners

    Article • April 2004, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen

  11. Prediction of Spectrum Fatigue Crack Growth in Latest Generation High Damage Tolerance Alloys

    Article • April 2004, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen

  12. Optimizing New Aluminum Alloys Through Computer Simulation

    Article • April 2003, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen

  13. Monolithic Structure: Materials and Methods for Reduced Cost, Reduced Weight and Improved Damage Tolerance

    Article • April 2003, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen

  14. On Material Models for Static Sizing of Compression Driven Airframe Structure

    Article • April 2002, American Institute of Aeronautics and Astronautics (AIAA)

    ir Sjoerd O van der Veen