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Prof.Dr. ALTAN KAYRAN
FACULTY OF ENGINEERING
PublicationsResearchMembership & Awards
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Phone :  +90312210 2433
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Education

  Bachelor's, Middle East Technical University, Mechanical Eng.
  Doctorate, University of Delaware, Mechanical And Aerospace Eng.

Publications (INTERNATIONAL)

Journal Papers

  A.1 Altan KAYRAN, Flutter qualification of transport aircraft with store suspension. "Aircraft Engineering and Aerospace Technology", 76, (2004), p.19-28.
  A.2 Altan Kayran, Küssner's Function in the Sharp-Edged Gust Problem-A Correction. "Journal of Aircraft", 43, (2006), p.1596-1598.
  A.3 Altan Kayran, Flight flutter testing and aeroelastic stability of aircraft. "Aircraft Engineering and Aerospace Technology", 79, (2007), p.150-162.
  A.4 Altan Kayran and Erdem Yavuzbalkan, Semi-analytical study of free vibration characteristics of shear deformable filament wound anisotropic shells of revolution. "Journal of Sound and Vibration", 319, (2009), p.260-281.
  A.5 İlke Aydıncak and Altan Kayran, An approach for the evaluation of effective elastic properties of honeycomb cores by finite element analysis of sandwich panels. "Journal of Sandwich Structures and Materials", 11, (2009).
  A.6 Kayran, A., Yavuzbalkan, E.,, Free vibration analysis of ring-stiffened branched composite shells of revolution. "AIAA Journal", 48, (2010), p.749-762.
  A.7 Konokman, HE., Çoruh, MM., and Kayran A.,, Computational and experimental study of high speed impact of metallic Taylor cylinders. "ACTA Mechanica", 220, (2011), p.61-85.
  A.8 Kayran, A., İbrahimoğlu, CS.,, Effect of semi-geodesic winding on the vibration characteristics of filament wound shells of revolution. "Journal of Applied Mechanics", 78, (2011), p.061008(1-11).
  A.9 Murat Günel and Altan Kayran, Non-Linear Progressive Failure Analysis of Open-Hole Composite Laminates Under Combined Loading. "Journal of Sandwich Structures and Materials", 15, (2013), p.309-339.
  A.10 M. Burak Sayar and Altan Kayran, ‘Two Stage Fatigue Life Evalution of and Aircraft Fuselage Panel with a Circumferential Crack and a Broken Stringer. "Fatigue and Fracture of Engineering Materials and Structures", (2013), p.1-13.
  A.11 Sayar, Burak; Kayran, Altan, Two Stage Fatigue Life Evalution of Aircraft Fuselage Panel with a Bulging Circumferential Crack and a Broken Stringer. "Fatigue and Fracture of Engineering Materials and Structures", 37, (2014), p.494-507.
  A.12 Dababneh, Odeh., Kayran, Altan, Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. "International Journal of Structural Integrity", 5, (2014), p.214 – 226.
  A.13 Kerem Furkan Çiçek, Merva Erdal, Altan Kayran, Experimental and Numerical Study of Process-Induced Total Spring-in of Corner-Shaped Composite Parts. "Journal of Composite Materials", (2016).
  A.14 Okan Çınar, Merve Erdal, Altan Kayran, Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior. "Journal of Sandwich Structures and Materials", 19, (2017), p.139–166.
  A.15 Hüseyin EmrahKonokman, Altan Kayran, Mustafa Kaya, Aircraft vulnerability assessment against fragmentation warhead. "Aerospace Science and Technology", 67, (2017), p.215-227.
  A.16 Kerem Furkan Çiçek, Merve Erdal, Altan Kayran, Experimental and numerical study of process-induced total spring-in of corner-shaped composite parts. "Journal of Composite Materials", 51, (2017), p.2347–2361.
 

Conference Papers

  A.1 Altan KAYRAN, Aeroelastic Stability of a Transport Aircraft With Wing Mounted Store Suspension-Part II: Flight Test. "7th Biennial Conference on Engineering Systems Design and Analysis", CD-ROM, (2004), p.1-11.
  A.2 Altan KAYRAN, Aeroelastic Stability of a Transport Aircraft With Wing Mounted Store Suspension-Part I: Analysis. "7th Biennial Conference on Engineering Systems Design and Analysis", CD-ROM, (2004), p.1-11.
  A.3 Altan Kayran and Erdem Yavuzbalkan, Effect of Anisotropy on the Vibration Characteristics of Composite Shells of Revolution. " Proceedings of 16th International Conference on Composite Materials- ICCM-16-Kyoto", CD ROM, (2007).
  A.4 Altan Kayran and Erdem Yavuzbalkan, Numerical Integration Based Vibration Analysis of Anisotropic Branched Shells of Revolution with Ring Stiffeners. "Proceedings of 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", CD ROM, (2007), p.AIAA 2007-2114.
  A.5 Altan Kayran, Free Vibration Characteristics of Composite Shells of Revolutıon with Variable Stiffness Coefficients. "ESDA08, 9th Biennial Conference on Engineering Systems Design and Analysis, Haifa, Israel", CD ROM, (2008), p.CD ROM.
  A.6 Sinan Oygür and Altan Kayran, Numerical Integration Based Approach to the Analysis of Anisotropic Shells of Revolution Subjected to Non-Axisymmetric Loading. "Proceedings of 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", CD-ROM, (2009), p.AIAA 2009-2346.
  A.7 Altan Kayran and İlke Aydıncak, Assessment of Effective Elastic Properties of Honeycomb Cores by Finite Element Analysis of Sandwich Panels. "Proceedings of 17th International Conference on Composite Materials- ICCM-17, Edinburgh,UK", CD-ROM, (2009).
  A.8 Sercan Soysal, Altan Kayran, Engin Şenelt and Nafiz Alemdaroğlu, Composite Manufacturing of the Wing of a Tactical Unmanned Air Vehicle. "7th International Conference on Composite Science and Technology, United Arab Emirates", CD-ROM, (2009).
  A.9 Sercan Soysal, Altan Kayran and Nafiz Alemdaroğlu, Structural Analysis of the Sandwich Composite Wing of a Tactical Unmanned Air Vehicle. "7th International Conference on Composite Science and Technology, United Arab Emirates", CD-ROM, (2009).
  A.10 Kayran, A., İbrahimoğlu, CS.,, Investigation of the Effect of Friction on the Stiffness and Vibration Characteristics of Filament Wound Composite Shells of Revolution. "ICCS 16, 16th International Conference on Composite Structures", (2011).
  A.11 Özöztürk, S., S.Ö, Kayran, A., Alemdaroğlu, N., Seber, G.,, On the Design and Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle. "52th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", (2011), p.AIAA-2011-1918.
  A.12 Günel, M., Kayran, A.,, Comparative Study of Linear and Non-Linear Progressive Failure Analysis of Composite Aerospace Structures. "ICCS 16, 16th International Conference on Composite Structures", (2011).
  A.13 Sayar, B., Kayran, A., Comparison of Stress Intensity Factor Calculations in Cracked Sheets with Riveted Stringers by Analytical and Finite Element Method. "2nd International Conference of Engineering Against Fracture (ICEAF II), Mykonos, GREECE", (2011).
  A.14 Kayran, A.,, Wind turbine components and materials. "International 100% Renewable Energy Conference and Exhibition (IRENEC 2011), İstanbul, Turkey", (2011).
  A.15 Günel, M., Kayran, A.,, Non-Linear Progressive Failure Analysis of Composite Aerospace Structures. "ICCM 18, 18th International Conference on Composite Materials, Jeju Island, Korea", (2011).
  A.16 Günel, M., and Kayran, A., Linear and Nonlinear Progressive Failure Analysis of Composite Aerospace Structures Under Combined Loading. " Proceedings of 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", (2012), p.AIAA-2012-1860.
  A.17 Özcan, G., Özöztürk, S., Senelt, E., Kayran, A., Alemdaroğlu, N, Aero-structural and Integrated Circuit Design of a Twin Wing-Tail Boom Configuration Tactical UAV. "2012 International Conference on Unmanned Aircraft Systems (ICUAS'12)", (2012).
  A.18 Kayran, A., Yavuzbalkan, E., and İbrahimoğlu, S, Investigation of the Effect of Geodesic and Semi-geodesic Winding on the Vibration Characteristics of Variable Stiffness Filament Wound Shells of Revolution. " Proceedings of 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", (2012), p.AIAA-2012-1472.
  A.19 Sayar, M.B., Kayran, A, Two Stage Damage Tolerance Evalution of and Aircraft Fuselage Panel with a Circumferential Crack and a Broken Stringer. "Proceedings of 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference", (2013), p.AIAA 2013-1478.
  A.20 Dababneh, O., Kayran, A., Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. "3rd EASN Association International Workshop on AeroStructures", (2013).
  A.21 Gözcü, M.Ozan; Kayran, Altan, Investigation of the effect of bending-twisting coupling on the load in wind turbines with superelement blade definition. "The Science of Making Torque from Wind 2014 - J. Phys.: Conf. Ser.", 524, (2014).
  A.22 Kayran, Altan; İbrahimoğlu C.Serkan, Preliminary study on the applicability of semi-geodesic winding in the design and manufacturing of composite towers. " J. Phys.: Conf. Ser. (2014)", 555, (2014).
  A.23 Nalcı, M.Ozan; Kayran, Altan, Aeroservoelastic Modelling and Analysis of a Missile Control Surface with a Nonlinear Electromechanical Actuator. "AIAA Atmospheric Flight Mechanics Conference, AIAA Aviation and Aeronautics Forum and Exposition", AIAA, (2014), p.AIAA 2014-2055.
  A.24 Gözcü, M.Ozan; Olgun, M.Nisa; Kayran, Altan, Investigation of the effect of off-axis spar cap plies on damage equivalent loads in wind turbines with superelement blade definition. "AIAA Science and Technology Forum and Exposition 2014", AIAA, (2014), p.AIAA 2014-1223.
  A.25 Sargın, Hakan; Kayran, Altan, Comparison of transient and quasi-steady aeroelastic analysis of wind turbine blade in steady wind conditions. "The Science of Making Torques from Wind 2014 - J. Phys.: Conf. Ser.", 524, (2014).
  A.26 Konokman Emrah,H; Kayran, Altan; Kaya, Mustafa, Analysis of Aircraft Surviability Against Fragmenting Warhead Threats. "AIAA Science and Technology Forum and Exposition 2014", AIAA, (2014), p.AIAA 2014-0355.
  A.27 Gözcü, M.O., Farsadi,T., Şener, Ö., Kayran, A, Assessment of the Effect of Hybrid GFRP-CFRP Usage in Wind Turbine Blades on the Reduction of Fatigue Damage Equivalent Loads in the Wind Turbine System. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 33rd Wind Energy Symposium", (2015), p.AIAA 2015-0999.
  A.28 Gözcü, M.O., Farsadi,T., Şener, Ö., Kayran, A.,, Reduction of Fatigue Damage Equivalent Loads in the Wind Turbine System Through the Use of Off-Axis Plies in the Spar Caps of Composite Wind Turbine Blades. "20th International Conference on Composite Materials -ICCM 20", (2015).
  A.29 Yılmaz, SE, Özcilhan T., Kayran, A., Gürses, E., Çoker, D.,, Design of Experiments Study for Determination for the Study of the Effect of Contact Parameters in Bolted Flange Connection. "International Conference on Advances in Mechanical Engineering, İstanbul 2015-ICAME’15", (2015).
  A.30 Özgün Şener, Touraj Farsadi, M. Ozan Gözcü, Altan Kayran, Reduction of fatigue damage equivalent loads In the wind turbine system through the use bending-twisting coupling induced in composite wind turbine blades. "EERA JP-Wind/IRPWIND konferansı", (2015).
  A.31 Güldü, S., Kayran, A.,, Maximizing Buckling Load Factors of Fiber-Placed Composite Cylindrical Shells by Particle Swarm Optimization. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 56th AIAA/ASCE/AHS/ASC Structur", (2015), p.AIAA 2015-0449.
  A.32 Yıldırım, A., Akay, AA, Gülaşık, H., Çoker, D., Gürses, E., Kayran, A.,, Parameters Correlation Study to Investigate the Effects of Geometric Variables on the Safety of Bolted Flange Connections. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-1107.
  A.33 Akay, AA, Gülaşık, H., Yıldırım, A., Çoker, D., Kayran, A., Gürses, E.,, Modeling of Circular Double Flange Joint Including Contact and Friction Effects. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-1201.
  A.34 Touraj Farsadi and Altan Kayran, Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades. "11th EAWE PhD Seminar on Wind Energy in Europe Session: Rotor Dynamics and Aerodynamics", (2015), p.Paper 73492.
  A.35 Yıldırım, A., Akay, AA, Gülaşık, H., Çoker, D., Gürses, E., Kayran, A.,, Development of bolted flange design tool based on finite element analysis and artificial neural network. "Proceedings of the ASME 2015 International Mechanical Engineering Congress and Exposition IMECE2015", (2015), p.IMECE2015-51021.
  A.36 Mert, B., Kayran, A.,, Post-Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-116.
  A.37 Yılmaz, SE, Kayran, A., Gürses, E., Çoker, D.,, Parametric Study for the Study of the Effect of Contact Parameters for Plastic Analysis of Bolted Flange Connections. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-1068.
  A.38 Özöztürk S., Kayran, A., Tuncer IH.,, Fluid Structure Interaction Based on Panel Method and Geometrically Nonlinear Structural Analysis. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-159.
  A.39 Şener, Ö., Farsadi,T., Gözcü, M.O., Kayran, A.,, Utilizing Bending-Twisting Coupling in Composite Wind Turbine Blades in Achieving Reduction in Fatigue Loads. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-069.
  A.40 Bartan, B., Kayran, A., Acar, B.,, Parametric Study of Delamination Analysis in Composites with Cohesive Zone Method. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-078.
  A.41 Dede, O., Kayran, A.,, Investigation of Effects of Bird Strike on Wing Leading Edge By Using Explicit Finite Element Method. "8th Ankara International Aerospace Conference-AIAC", (2015), p.AIAC-2015-138.
  A.42 Touraj Farsadi, Altan Kayran, Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2016", (2016), p.AIAA 2016-1959.
  A.43 Touraj Farsadi, Altan Kayran, Aeroelastic Stability Evaluation of Bend-Twist Coupled Composite Wind Turbine Blades Designed for Load Alleviation in Wind Turbine Systems. "AIAA 2016-1009, AIAA Science and Technology Forum and Exposition, AIAA SciTech 2016", (2016), p.AIAA 2016-1009.
  A.44 Mesut Mert, Altan Kayran, Post-Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2016", (2016), p.AIAA 2016-1974.
  A.45 Büşra Bartan, Bülent Acar, Altan Kayran, Three Dimensional Delamination Analysis in Composite Open Hole Tensile Specimens with Cohesive Zone Method. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2016", (2016), p.AIAA 2016-0980.
  A.46 Meryem Nisa Ataç, Altan Kayran, Comparative Study of Finite Element Analysis and Geometrically Exact Beam Analysis of a Composite Helicopter Blade. "American Helicopter Society AHS 72nd Annual Forum", (2016).
  A.47 Ayberk Alperen Işık, Altan Kayran, Structural Optimization of Composite Helicopter Rotor Blades. "American Society for Composites, 31st Technical Conference and ASTM Committee D30 Meeting", (2016).
  A.48 Touraj Farsadi, Altan Kayran, Structural Dynamics Analysis and Passive Control of Wind Turbine Vibrations with Tuned Mass Damper (TMD) Technique. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2016", (2016), p.AIAA 2016-1481.
  A.49 Uğur Hayırlı, Altan Kayran, Stick Model Development of Aircraft Structures for Dynamic Analysis. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2017", AIAA 2017, (2017).
  A.50 Latif Kesemen, Altan Kayran, High Strain Rate Material Characterization of Al 7075-T651 by Modified Taylor Impact Test and Velocity Interferometry. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2017", AIAA 2017, (2017).
  A.51 Enes Aydın Altan Kayran, Investigation of the Effect of Boundary Conditions on the Buckling Coefficients of Stiffened Flat Panels. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.52 Touraj Farsadi, Özgün Şener, Altan Kayran, Free Vibration Analysis of Uniform and Asymmetric Composite Pretwisted Rotating Thin Walled Beam. "ASME 2017 International Mechanical Engineering Congress and Exposition, IMECE 2017", IMECE2017, (2017).
  A.53 Gülce Öztürk Altan Kayran, Energy Absorption Mechanisms and Crash Analysis of Helicopter Seats. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.54 İsmail Gürzap Demirel Altan Kayran, The Effect of Modal Damping on Random Vibration Metal Fatigue Analysis. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.55 Ahmet Arda Akay, Hasan Gülaşık, Demirkan Çoker, Altan Kayran, Ercan Gürses, Experimental Study and Finite Element Analysis of Dovetail Attachments. "ASME 2017 International Mechanical Engineering Congress and Exposition, IMECE 2017", IMECE2017, (2017).
  A.56 Touraj Farsadi, Özgün Şener, Altan Kayran, Effect of Fibre Orientation of Bend-Twist Coupled Blades on the Structural Performance of the Wind Turbine System. "AIAA Science and Technology Forum and Exposition, AIAA SciTech 2017", AIAA 2017, (2017).
  A.57 Hasan İnci Altan Kayran, Design Optimization of Variable Stiffness Composite Laminates Using Surrogate Models for Compliance and Buckling Load. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.58 Can Serkan İbrahimoğlu, Altan Kayran, Stress and Deformation Analysis of Anisotropic Shells of Revolution Wound Using Semi-Geodesic Fiber Paths. "ICCS20, 20th International Conference on Composite Structures", (2017).
  A.59 Bali İhsan Özturan Altan Kayran, Multibody Simulation of Helicopter Rotor with Flexible Blade. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.60 Mert Atasoy Altan Kayran, Comparison of 2D and 3D Homogenization Processes for Micromechanics Analysis of Unidirectional Composites. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.61 Oğuz Atalay Touraj Farsadi Altan Kayran, Performance Study of Wind Turbines with Bend-Twist Coupled Blades at Underrated Wind Speeds. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.62 Özge Özkaya Altan Kayran, Nonlinear Static Aeroelastic Behaviour of Composite Missile Fin with Interlaminar Damage. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.63 Ahmet Arda Akay, Demirkan Çoker, Altan Kayran, Ercan Gürses, Implementation of the Submodelling Technique on the Dovetail Attachments. "9th Ankara International Aerospace Conference-AIAC", (2017).
  A.64 Volkan Sanlı, Ercan Gürses, Demirkan Çoker, Altan Kayran, Development of Artificial Neural Network Based Design Tool for Aircraft Engine Bolted Flange Connection Subject to Combined Axial and Moment Load. "ASME 2017 International Mechanical Engineering Congress and Exposition, IMECE 2017", IMECE2017, (2017).
  A.65 Ömer Erdolu, Altan Kayran, Damage Analysis in Blast Loaded Concrete Columns Using Single Degree of Freedom Approach. "17th International Symposium on the interaction of the Effects of Munitions with Structures- ISIEMS", (2017).

Publications (NATIONAL)

 

Journal Papers

  A.1 T.Turgut, A.Kayran, N. Alemdaroğlu, Mç Ceylan, Vakum Torbalama Yöntemi ile Kompozit Malzemeden Yapı Üretimi Örnek bir Havacılık Uygulamazı. "TMMOB Mühendis ve Makina", (2007).
 

Conference Papers

  A.1 Caner Taş, Yavuz Yaman, Altan Kayran, HAVA TAŞITLARINA UYGULANAN GÜÇLENDİRİLMİŞ SİLİNDİRİK BİR DIŞ DEPONUN YAPISAL ANALİZİ. "11. Ulusal Makina Teorisi Sempozyumu", 2, (2003), s.469-480.
  A.2 Altan Kayran ve Erdem Yavuzbalkan, Lif sargılı silindirik kabuk yapılarının serbest titreşim analizi için sayısal bir yöntem. "II. Ulusal Mühendislik Kongresi, Zonguldak Karaelmas Universitesi, Zonguldak", (2006), s.329-339.
  A.3 Altan Kayran ve Erdem Yavuzbalkan, ÇEVRESEL GÜÇLENDİRİLMİŞ DALLI ANİZOTROPİK KABUK YAPILARININ TİTREŞİM ANALİZİ İÇİN BİR YÖNTEM. "I. ULUSAL HAVACILIK VE UZAY KONFERANSI, ODTÜ, Ankara", CD-ROM, (2006), s.UHUK-2006-041.
  A.4 Emrah Konokman, Altan Kayran and Yusuf Özyörük, Lagrangian Hyrdocode Formulation for Large Deformation Problems and Methods to Prevent Volumetric Locking of Triangular Elements. "4th Ankara International Aerospace Conference-AIAC", CD ROM, (2007), s.AIAC-2007-072.
  A.5 Efe Kafdağlı and Altan Kayran, Development of a Sabot Design Tool for Aeroballistic Range Testing. "4th Ankara International Aerospace Conference-AIAC", CD ROM, (2007), s.AIAC-2007-032.
  A.6 Altan Kayran, General Review of Aeroelastic Stability Flight Testing. "4th Ankara International Aerospace Conference-AIAC", CD ROM, (2007), s.AIAC-2007-025.
  A.7 Tahir Turgut and Altan Kayran, Structural Analysis of a Lightweight Composite Wing and Material Characterization. "4th Ankara International Aerospace Conference-AIAC", CD ROM, (2007), s.AIAC-2007-027.
  A.8 Erdem Yavuzbalkan ve Altan Kayran, Çok katmanlı kompozit yapıdaki kanat kutularının basitleştirilmiş yapısal analizi için bir yöntem. "II. Ulusal Havacılık ve Uzay Konferansı, İTÜ, İstanbul", CD ROM, (2008), s.CD ROM.
  A.9 Mustafa Ekren and Altan Kayran, Structural Optimization of Wing Torque Boxes Using Different Idealizations in the Finite Element Model. "5th Ankara International Aerospace Conference-AIAC, Ankara", CD-ROM, (2009), s.AIAC-2009-120.
  A.10 Emrah Konokman and Altan Kayran, Hydrocode Analysis and Experimental Verification of Taylor Impact Tests. "5th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", CD-ROM, (2009), s.AIAC-2009-063.
  A.11 Yücel Devellioğlu and Altan Kayran, Electronic Packaging and Environmental Test and Analysis of an Electronic Unit. "5th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", CD-ROM, (2009), s.AIAC-2009-041.
  A.12 Serhan Yüksel, Altan Kayran and Nafiz Alemdaroğlu, Kompozit bir Mini İnsansız Hava Aracının Gövde Üzerine Düşük Hızlı Darbeli İnme Analizleri. "USMOS 2009, Ulusal Savunma Uygulamaları Modelleme ve Simülasyon Konferansı", USB bellek, (2009).
  A.13 Altan Kayran, Sercan Soysal and Nafiz Alemdaroğlu, Co-cured and Secondary Bonding Method of Manufacturing Multi-Cell Box Beam and Wing Structures and by Vacuum Infusion and Vacuum Bagging Processes. "5th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", CD-ROM, (2009), s.AIAC-2009-030.
  A.14 Altan Kayran and İlke Aydıncak, Assessment of Effective Elastic Properties of Honeycomb Cores by Finite Element Analysis of Sandwich Panels via ANSYS. "14th Conference for Computer Aided Engineering and System Modeling, METU, Ankara", CD-ROM,, (2009).
  A.15 Senelt, E., Kayran, A, ve Alemdaroğlu, N.,, Bir taktik insansız hava aracının kompozit gövde kalıbı ve kompozit gövde üretimi. "2. Ulusal Havacılık ve Uzay Konferansı", (2010), s.CD.
  A.16 Özöztürk, S., Kayran, A., Alemdaroğlu, N., Seber, G, Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-070.
  A.17 Dababneh, O., Kayran, A.,, Structural Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Types of Finite Elements in the Preliminary Design Phase. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-064.
  A.18 Dababneh, O., Kayran, A.,, Design and Analysis of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-066.
  A.19 Sayar, B., Kayran, A.,, Determination of Stress Intensity Factors in Cracked Sheets with Riveted Stringers by Analytical and Finite Element Method. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-074.
  A.20 Özöztürk, S., Kayran, A., Alemdaroğlu, Computational Aerodynamics and Structural Analysis of a Fully Compozite Twin Wing-Tail Boom Configuration Unmanned Air Vehicle. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-071.
  A.21 İbrahimoğlu, S., Kayran, A.,, Investigation of the Effect of Preset Friction on the Stiffness and Vibration Characteristics of Filament Wound Composite Shells of Revolution. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-055.
  A.22 Günel, M., Kayran, A.,, Comparative Study of Linear and Non-Linear Progressive Failure Analysis of Composite Aerospace Structures. "6th Ankara International Aerospace Conference-AIAC, Ankara, Turkey", (2011), s.AIAC-2011-069.
  A.23 Demircan, A., Kurtuluş, D.F., ve Kayran, A., Kompozit Yapılı Mini İHA'lar için Kalıp Üretim Teknikleri ve Aerodinamik Yüzeylerin Üretimi. "IV. Ulusal Havacılık ve Uzay Konferansı", (2012).
  A.24 Atasoy, M., ve Kayran, A, Civatalı Bağlantılarda Kanırtma Kuvvetlerinin Belirlenmesi. "IV. Ulusal Havacılık ve Uzay Konferansı", (2012).
  A.25 Tola, C., Kayran, A.,, The Effect of Fiber Orientation Angle on Subsonic and Supersonic Flutter Characteristics of a Composite Missile Fin’. "7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-012.
  A.26 Güldü, S., Kayran, A., Tursun G., Koçkar, A.,, Two Level Optimization of Fiber Placed Laminated Cylindrical Shells of Revolution’. "7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-1127.
  A.27 İbrahimoğlu, CS., Kayran, A.,, Semi-geodesic Winding of Composite Conical Shells – Possible Application for Composite Towers. "RUZGEM 2013, Conference on Wind Energy Science and Technology", (2013), s.RZGM2013-3.
  A.28 Nalcı, M.O., Kayran, A.,, Development of an Aeroservoelastic Mathematical Model of a Missile Control Fin. "7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-125.
  A.29 Atasoy, M., Kayran, A.,, Determination of Prying Loads on Bolted Connections. " 7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-119.
  A.30 Yeniceli, S.C., Kayran, A.,, Design Optimization of a Whiffletree System for Static Testing of a Wind Turbine Blade. "RUZGEM 2013, Conference on Wind Energy Science and Technology", (2013), s.RZGM2013-59.
  A.31 Gözcü, M.O., Olgun, M.N., Kayran, A.,, Inverse Design of 3D Reference Wind Turbine Blades To Study Bending-Twisting Coupling Effect on Load Alleviation. "RUZGEM 2013, Conference on Wind Energy Science and Technology", (2013), s.RZGM2013-8.
  A.32 İnci, H., Kayran, A., ‘, Continuous Fiber Path Optimization in Composite Structures. "7th Ankara International Aerospace Conference-AIAC", (2013), s. AIAC-2013-074.
  A.33 Nalcı, M.O., Kayran, A.,, Aeroelastic and Control System Modeling of a Missile Control Fin for Aeroservoelastic Analysis’. "7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-124.
  A.34 Balevi, S., Kayran, A., Simulated Flutter Test of Wings. "7th Ankara International Aerospace Conference-AIAC", (2013), s. AIAC-2013-011.
  A.35 Konokman E.H, Kayran, A., Kaya, M.,, Survivability Analysis of Aircraft under Fragmentation Warhead Threat’. "7th Ankara International Aerospace Conference-AIAC", (2013), s.AIAC-2013-1156.
  A.36 Gözcü, M.O., Olgun, M.N., Kayran, A.,, Effect of Off-Axis Plies on the Damage Equivalent Loads in Wind Turbines with Superelement Blade Definition. " RUZGEM 2013, Conference on Wind Energy Science and Technology", (2013).
  A.37 Dede, Oğuzhan; Kayran, Altan, Kanat Hücum Kenarına Kuş Çarpma Probleminin Farklı Açık Sonlu Elemanlar Çözüm Yöntemleriyle İncelenmesi. "V. Ulusal Havacılık ve Uzay Konferansı", UHUK-2014, (2014), s.UHUK-2014-064.
  A.38 Ezgi Akel, Volkan Kargın, Altan Kayran, Helikopter pallerinin burulma yönünde elastik modellenmesi ve elastik modelin uçuş mekaniği analizlerine etkisi. "VI. Ulusal Havacılık ve Uzay Konferansı, UHUK 2016", (2016), s.UHUK-2016-010.
  A.39 Semih Soğancı, Altan Kayran, İsmail Hakkı Tuncer, Helikopter pallerinin çoklu kütleli benzetim aracı ve iki boyutlu panel tabanlı akış çözücüsü ile etkileşimli analizi. "VI. Ulusal Havacılık ve Uzay Konferansı, UHUK 2016", (2016), s.UHUK-2016-128.
  A.40 Uğur Hayırlı, Altan Kayran, Helikopter alt yapılarının dinamik analizi için düşük derecede modelleme. "VI. Ulusal Havacılık ve Uzay Konferansı, UHUK 2016", (2016), s.UHUK-2016-1095.
  A.41 Bertan Arpacıoğlu, Altan Kayran, Alüminyum bir helikopter yatay kuyruk kanadının yapısal tasarımı ve optimizasyonu. " VI. Ulusal Havacılık ve Uzay Konferansı, UHUK 2016", (2016), s.UHUK-2016-1052.
  A.42 Volkan Sanlı, A. Akay, A. Yıldırım, Ercan Gürses, Demirkan Çoker, Altan Kayran, Eksenel, kesme ve moment yükü altındaki flanşlar için yapay sinr apına dayalı civatalı flanş tasarım aracı geliştirilmesi. "VI. Ulusal Havacılık ve Uzay Konferansı, UHUK 2016", (2016), s.UHUK-2016-1055.
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