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  1. An Experimental Study of Added Mass on a Plunging Airfoil Oscillating with High Frequencies at High Angles of Attack

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

    Assistant professor Mohamed Y. Zakaria, click here www.qez8.f1s2.xyz qOPVwnynKGTF

  2. Nonlinear airfoil torsional response induced by separated flows

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

    click here www.qez8.f1s2.xyz qOPVwnynKGTF