All Stories

  1. Maximization of Ultimate Strength of Unidirectional Tapered Composite Structures Considering Different Failure Modes

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

    Ozan Çelik

  2. Fatigue Assessment of a Helicopter Rotor Blade Using Uniaxial and Multiaxial Fatigue Criteria

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

    Ozan Çelik, Alperen Ayberk IŞIK