All Stories

  1. Structural Response of a Stitched Composite Hybrid Wing Body Center Section

    Article • Journal of Aircraft, May 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Adam Przekop

  2. Lessons Learned from Large-Scale Aerospace Structural Testing

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

    Adam Przekop

  3. Modeling and Sensitivity Analysis of Sandwich Composite Cylinders with Geometric Imperfections

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

    Adam Przekop

  4. Design of a Manufacturing Demonstration Unit for a Composite Lunar Landing Gear Strut

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

    Adam Przekop

  5. Design of Buckling-Critical Large-Scale Sandwich Composite Cylinder Test Articles

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Adam Przekop

  6. Testing of a Stitched Composite Large-Scale Pressure Box

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

    Adam Przekop

  7. Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part I: Ultimate Design Loads

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

    Adam Przekop

  8. Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part II: Severe Damage

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

    Adam Przekop

  9. Imparting Barely Visible Impact Damage to a Stitched Composite Large-Scale Pressure Box

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

    Adam Przekop

  10. Vibroacoustic Tailoring of a Rod-Stiffened Composite Fuselage Panel with Multidisciplinary Considerations

    Article • Journal of Aircraft, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Albert Allen, Adam Przekop

  11. Warping of Stiffened Composite Panels Due to Temperature Changes in the Curing Process

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

    Mark Agate, Adam Przekop

  12. Nonlinear Finite Element Analysis of a Composite Non-Cylindrical Pressurized Aircraft Fuselage Structure

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

    Adam Przekop