All Stories

  1. Aeroelastic Model Corrections of a Very Light Aircraft

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

    Gul Demirer, Altan Kayran

  2. Flutter Optimization of a Wing–Engine System with Passive and Active Control Approaches

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

    Altan Kayran, Davood Asadi

  3. Experimental Assessment of Bend-Twist Coupling Potentials of Composite Materials via Digital Image Correlation Method

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

    Altan Kayran

  4. Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior

    Article • Journal of Sandwich Structures & Materials, March 2017, SAGE Publications

    Altan Kayran

  5. Effect of Fiber Orientation of Bend-Twist Coupled Blades on the Structural Performance of the Wind Turbine System

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

    Altan Kayran

  6. Stick Model Development of Aircraft Structures for Dynamic Analysis

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

    Altan Kayran

  7. High Strain Rate Material Characterization of Al 7075-T651 by Modified Taylor Impact Test and Velocity Interferometry

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

    Altan Kayran

  8. Experimental and numerical study of process-induced total spring-in of corner-shaped composite parts

    Article • Journal of Composite Materials, September 2016, SAGE Publications

    Altan Kayran

  9. Three-Dimensional Delamination Analysis in Composite Open Hole Tensile Specimens with Cohesive Zone Method

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

    Altan Kayran

  10. Aeroelastic stability evaluation of bend-twist coupled composite wind turbine blades designed for load alleviation in wind turbine systems

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

    Touraj Farsadi, Altan Kayran

  11. Structural dynamics analysis and passive control of wind turbine vibrations with Tuned Mass Damper (TMD) technique

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

    Touraj Farsadi, Altan Kayran

  12. Classical aeroelastic stability analysis of large composite wind turbine blades

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

    Touraj Farsadi, Altan Kayran

  13. Post-Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures

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

    Altan Kayran

  14. Maximizing Buckling Load Factors of Fiber-Placed Composite Cylindrical Shells by Particle Swarm Optimization

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

    Altan Kayran

  15. Assessment of the Effect of Hybrid GRFP-CFRP Usage in Wind Turbine Blades on the Reduction of Fatigue Damage Equivalent Loads in the Wind Turbine System

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

    Touraj Farsadi, Altan Kayran

  16. Design, analysis and optimization of thin walled semi-monocoque wing structures using different structural idealization in the preliminary design phase

    Article • International Journal of Structural Integrity, August 2014, Emerald

    Altan Kayran

  17. Aeroservoelastic Modeling and Analysis of a Missile Control Surface with a Nonlinear Electromechanical Actuator

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

    Altan Kayran

  18. Analysis of Aircraft Survivability Against Fragmenting Warhead Threat

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

    Dr. Mustafa Kaya, Altan Kayran

  19. Investigation of the effect of off-axis spar cap plies on damage equivalent loads in wind turbines with superelement blade definition

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

    Altan Kayran

  20. Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer

    Article • Fatigue & Fracture of Engineering Materials & Structures, November 2013, Wiley

    Altan Kayran