All Stories

  1. Investigation of an Axis-Symmetric Mach 5 Glass Blown Nozzle for Supersonic Optical Diagnostics.

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

    Charles Fabijanic, Al Habib Ullah

  2. Dynamic Stall Flow Structure During Pitching of Moderate Swept Finite-Aspect Ratio Wing

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

    Al Habib Ullah

  3. Background Oriented Schlieren Techniques in an Axis-Symmetric Glass Blown Mach 5 Nozzle.

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

    Al Habib Ullah, Joshua Yurek, Charles Fabijanic

  4. Experimental Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing

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

    Al Habib Ullah

  5. Design and Characterization of Optically Clear PMMA/ GOx Hybrid Rocket Propulsion System.

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

    Al Habib Ullah, Joshua Yurek, David Arstein

  6. Advanced Measurements and Analyses of Flow Past Three-Cylinder Rotating System

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

    Al Habib Ullah

  7. Experimental Evaluation of the Performance of Parabolic Flaps

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

    Douglas F Hunsaker, Al Habib Ullah

  8. PIV Study of the Flow Interaction between a Three-Cylinder Rotating System and a downstream Dimpled Airfoil

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

    Al Habib Ullah